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Department of Civil Engineering                                                                NPIC




                                  !$> karviPaK truss edayeRbIviFIPaBrwgRkaj
                         Truss analysis using the stiffness method

enAkñúgemeronenH eyIgnwgBnül;BIeKalkarN_mUldæanénkareRbIR)as;viFIPaBrwgRkajsRmab;viPaKeRKOg
bgÁúM. viFIenHmanPaBsμúKsμajsRmab;karedaHRsayedayéd EtvasaksmsRmab;eRbICamYynwgkMuBüÚT½r.
enAkñúgemeronenHmanbgðajBI]TahrN_Gnuvtþn_eTAelI truss kñúgbøg;. bnÞab;mk eyIgnwgeRbIviFIenH
sRmab; truss kñúglMh. eyIgnwgerobrab;BIkarGnuvtþviFIenHsRmab;Fñwm nigeRKagenAemeroneRkay.

!$>!> eKalkarN_mUldæanénviFIPaBrwgRkaj (Fundamentals of the stiffness method)
         eKmanmeFüa)ayBIrsRmab;viPaKrcnasm<½n§edayeRbIviFIm:aRTIs. viFIPaBrwgRkajEdlRtUveRbI
enAkñúgemeronenH nigemeroneRkayCakarviPaKedayeRbIviFIbMlas;TI. viFIkmøaMg EdleKehAfaviFI
flexibility ¬Edlerobrab;enAkñúgkfaxNÐ 10-1¦ k¾GaceRbIedIm,IviPaKrcnasm<½n§ b:uEnþviFIenHminRtUv)an

bgðajenAkñúgesovePAenHeT. mUlehtucm,gKW eKGaceRbIviFIPaBrwgRkajsRmab;viPaKrcnasm<½n§kMNt;
edaysþaTic nigrcnasm<½n§minkMNt;edaysþaTic cMENkÉviFI flexibility RtUvkardMeNIrkarepSgsRmab;
krNInImYy²énkrNITaMgBIr. ehIyviFIPaBrwgRkajpþl;eGaybMlas;TI nigkmøaMgedaypÞal; cMENkÉ
viFI flexibility minpþl;eGaybMlas;TIedaypÞal;eT. elIsBIenH eKmanPaBgayRsYlsresrrUbmnþ
m:aRTIsEdlcaM)ac;sRmab;RbtþibtþikarkMuBüÚT½redayeRbIviFIPaBrwgRkaj ehIyenAeBleKeFVIvarYc eK
GacviPaKeRKOgbgÁúMedaykMuBüÚT½ry:agmanRbsiT§PaB.
         karGnuvtþviFIPaBrwgRkajTamTarnUvkarbMEbkeRKOgbgÁúMCaes‘rIén finite elements ehIyeK
RtUvkMNt;GtþsBaØaNeGaycMNuccugrbs;Ggát;Ca node. sRmab;karviPaK truss, finite element Ca
Ggát;nImYy²EdlpSMCa truss ehIy node CatMN. eKRtUvkMNt;lkçN³kmøaMg nigbMlas;TIrbs;Ggát;
nImYy² ehIyeKRtUveFVITMnak;TMngrvagkmøaMg nigbMlas;TIedayeRbIsmIkarlMnwgkmøaMgEdlsresrenA
Rtg; node. bnÞab;mk eKerobcMTMnak;TMngTaMgenH ¬sRmab;rcnasm<½n§TaMgmUl¦ CaRkumbBa©ÚlKña
EdleKeGayeQμaHfa structure stiffness matrix K. enAeBlEdleKbegáItm:aRTIsrYcehIy eKGac
kMNt;bMlas;TIrbs; node sRmab;bnÞúkenAelIrcnasm<½n§. enAeBlEdleKsÁal;bMlas;TIrYcehIy eK
GackMNt;kmøaMgkñúgrbs;eRKOgbgÁúMedayeRbITMnak;TMngrvagkmøaMg nigbMlas;TIsRmab;Ggát;.


 karviPaK truss edayeRbIviFIPaBrwgRkaj                                              T.Chhay   -464
mhaviTüal½ysMNg;sIuvil                                                viTüasßanCatiBhubec©keTskm<úCa

          munnwgbegáItdMeNIrkarsRmab;GnuvtþviFIPaBrwgRkaj CaCMhandMbUgeyIgcaM)ac;yl;dwgBIniym
n½y nigeKalKMnitmYycMnYn³
karkMNt;GtþsBaØaNrbs;Ggát; nig node³ CMhanmYyénCMhandMbUgkñúgkarGnuvtþviFIPaBrwgRkaj
KWkMNt;GtþsBaØaNGgát;rbs;rcnasm<½n§ nig node rbs;va. eyIgnwgkMNt;Ggát;edaybg;elxEdl
B½T§CMuvijedaykaer ehIyelxEdlB½T§CMuvijedayrgVg;kMNt;eGay node. ehIy eKk¾RtUvkMNt;cugCit
nigcugq¶ayrbs;Ggát;edayeRbIk,alRBYjEdlvacg¥úleTAcugq¶ay. ]TahrN_énkarkMNt;Ggát;
node nigTisedAsMrab; truss RtUv)anbgðajenAkñúgrUbTI 14-1a.




kUGredaenskl nigkUGredaenGgát;³ edaysarbnÞúk nigbMlas;TICaTMhMviucT½r enaHeKcaM)ac;RtUv
begáItRbB½n§kUGredaenedIm,IkMNt;TisedArbs;vaeGay)anRtwmRtUv. enATIenH eyIgnwgeRbIRbB½n§kUGr
edaenBIrRbePTepSgKña. RbB½n§kUGredaenskl b¤RbB½n§kUGredaenrcnasm<½n§ ¬ x, y ¦ RtUveRbIedIm,I
kMNt;TisedAénbnÞúkxageRkA nigTisedAénbgÁúM;bMlas;TIenARtg; node ¬rUbTI 14-1a¦. RbB½n§kUGr
edaentMbn; b¤RbB½n§kUGredaenGgát;RtUv)aneRbIsRmab;Ggát;nImYy²edIm,IkMNt;TisedAénbMlas;TI
rbs;va nigkmøaMgkñúgrbs;va. RbB½n§enHRtUv)ankMNt;edayeRbIG½kS x' , y' CamYynwgKl;enARtg;
node Cit ehIyG½kS x' latsn§wgeq<aHeTArk node q¶ay. ]TahrN_sRmab;Ggát; truss elx $ RtUv

)anbgðajenAkñúgrUbTI 14-1b.
PaBminkMNt;sIueNm:aTic³ dUckarerobrab;enAkñúgkfaxNÐ 11-1, degree of freedom Edlminman
karTb;sRmab; truss CaGBaØatdMbUgénviFIbMlas;TI dUcenHeKRtUvEtkMNt;va. tamc,ab;TUeTA eKman
degree of freedom b¤bMlas;TIEdlGacekItmancMnYnBIr sMrab;tMN (node). sRmab;karGnuvtþ

degree of freedom nImYy²RtUv)ankMNt;enAelI truss edayeRbIelxkUd ¬EdlbgðajenARtg;tMN b¤


Truss analysis using the stiffness method                                      T.Chhay   -465
Department of Civil Engineering                                                            NPIC



node  ¦ ehIyeKeRbI k,alRBYjedaysMGageTAelIkUGredaensklviC¢man. ]TahrN_ truss
enAkñúgrUbTI 14-1a man degree of freedom cMnYn8 EdlRtUv)ankMNt;;edayelxkUdBIelx 1 dl;
elx 8 dUcbgðaj. Truss enHminkMNt;edaysIueNm:aTicdWeRkTI5 edaysarbMlas;TIEdlGac
ekItmanTaMg 8enH elx1 dl;elx5 CaGBaØat b¤ degree of freedom EdlminmankarTb; ehIyelx
6 dl;elx8Ca degree of freedom EdlmankarTb;. edaysarmankarTb; bMlas;TIenATIenHRtUvesμI

sUnü. sRmab;karGnuvtþbnþbnÞab; eyIgeRbIelxkUdtUc²sRmab;sMKal;bMlas;TIEdleyIgminsÁal;
¬degree of freedom EdlminTb;¦ ehIyelxkUcFM²sRmab;sMKal;bMlas;TIEdlsÁal; ¬degree of
freedom EdlTb;¦. mUlehtukñúgkareFVIEbbenH edIm,IgayRsYlerobcM structure stiffness matrix

dUcenHeyIgnwgGackMNt;bMlas;TIEdlCaGBaØatedaypÞal;.
         eRkayeBleyIgbg;elxeGay truss ehIykMNt;elxkUd eyIgGacKNna structure
stiffness matrix K. edIm,IeFVIEbbenH dMbUgeyIgRtUvbegáIt member stiffness matrix k’ sRmab;

Ggát;nImYy²rbs; truss. eKeRbIm:aRTIsenHedIm,IbgáajTMnak;TMngrvagbnÞúk nigbMlas;TIrbs;Ggát;
edayeRbIkUGredaentMbn;. edaysarGgát;TaMgGs;rbs; truss minmanTisdUcKña eyIgRtUvbMElgTMhM
TaMgenHBIkUGredaentMbn; x' , y' eTACakUGredaenskl x, y edayeRbIm:aRTIsbMElgkmøaMg nig
bMlas;TI (force and displacement transformation matrices). eRkaybegáItrYcehIy eyIgGac
bMElgm:aRTIsPaBrwgRkajrbs;Ggát;BIkUGredaentMbn;eTACakUGredaenskl ehIybnÞab;mkpÁúMva
edIm,IbegáItCam:aRTIsPaBrwgRkajrcnasm<½n§. edayeRbI K ¬dUckarbgðajxagelI¦ dMbUgeyIgGac
kMNt;bMlas;TIrbs; node bnÞab;mkeyIgGackMNt;kmøaMgRbtikmμTMr nigcugeRkayKWkmøaMgkñúgrbs;
Ggát;. eyIgnwgbegáItviFIenH.

!$>@> m:aRTIsPaBrwgRkajrbs;Ggát; (Member stiffness matrix)
       enAkñúgkfaxNÐenH eyIgnwgbegáItm:aRTIsPaBrwgRkajsMrab;Ggát;eTalrbs; truss edayeRbI
kUGredaentMbn; x' , y' dUcbgðajenAkñúgrUbTI 14-2. tYenAkñúgm:aRTIsenHCaTMnak;TMngrvagbnÞúk nig
bMlas;TIsRmab;Ggát;.
       Ggát;rbs; truss Gacpøas;TI)anEttamG½kS x' rbs;vab:ueNÑaH edaysarbnÞúkGnuvtþtamTis
enH. dUcenH eKGacmanbMlas;TIÉkraCüBIr. enAeBleKeGaycugCitrbs;Ggát;manbMlas;TIviC¢man

 karviPaK truss edayeRbIviFIPaBrwgRkaj                                          T.Chhay   -466
mhaviTüal½ysMNg;sIuvil                                                  viTüasßanCatiBhubec©keTskm<úCa

dN  ehIycMENkÉcugq¶ayRtUv)anTb;edaysnøak; ¬rUbTI 14-2a¦ enaHkmøaMgEdlekItmanenARtg;
cugrbs;Ggát;KW
                    AE                                    AE
           q' N =      dN                      q' F = −      dN
                     L                                     L
cMNaMfa q' GviC¢manedaysarsßanPaBlMnwg vaRtUveFVIGMeBItamTisedAGviC¢man x' . dUcKña bMlas;TI
                F

viC¢man d enARtg;cugq¶ayedaycugCitenAEtTb;edaysnøak; ¬rUbTI 14-2b¦ pþl;nUvkmøaMgkñúgGgát;
            F
                         AE                               AE
            q' ' N = −      dF                 q' ' F =      dF
                          L                                L
edaykareFIVtRmYtpl ¬rUbTI 14-2c¦ kmøaMgers‘ultg;EdlbgáedaybMlas;TITaMgBI
                AE      AE
           qN =    dN −    dF                                                         (14-1)
                 L       L
                AE      AE
           qF =    dF −    dN                                                         (14-2)
                 L       L
eKGacsresrsmIkarTMnak;TMngrvagbnÞúk nigkmøaMgkñúgTRmg;m:aRTIs*Ca
           ⎡q N ⎤ AE ⎡ 1 − 1⎤ ⎡d N ⎤
           ⎢ q ⎥ = L ⎢− 1 1 ⎥ ⎢ d ⎥
           ⎣ F⎦      ⎣      ⎦⎣ F ⎦
b¤ q = k ' d                                                                (14-3)

Edl k ' = AE ⎡−11 −11⎤
               L ⎢      ⎥                                                   (14-4)
                  ⎣     ⎦
m:aRTIs k ' RtUv)aneKeGayeQμaHfam:aRTIsPaBrwgRkajsRmab;Ggát; ehIyvamanTRmg;dUcKñasRmab;
Ggát;nImYy²rbs; truss. tYTaMgbYnEdlbegáItCam:aRTIsenHRtUv)aneKeGayeQμaHfaemKuNT§iBl
kRmajsRmab;Ggát; (member stiffness influence coefficient) k' . k' CakmøaMgenARtg;tMN i
                                                                   ij   ij

enAeBltMN j ekItmanbMlas;TImYyÉktþa. ]TahrN_ RbsinebI i = j = 1 enaH k ' CakmøaMgenA11

Rtg;cugCit enAeBlcugq¶ayRtUv)anTb;edaybgáb; ehIycugCitrgbMlas;TI d = 1 eBalKW
                                                                         N
                             AE
           q N = k '11 =
                              L
dUcKña eKkMNt;kmøaMgenAcugq¶ayBI i = 2 /          j =1    dUcenH
                                AE
           q F = k ' 21 = −
                                 L
tYTaMgBIrenHCaCYrQrTImYyrbs;m:aRTIsPaBrwgRkajGgát;. tamrebobdUcKña CYrQrTIBIrrbs;m:aRTIs
enHCakmøaMgenAkñúgGgát;enAeBlcugq¶ayrbs;Ggát;rgbMlas;TIÉktþa.

*
    ]bsm<½n§ A pþl;eGaynUvkarrMlwkBIm:aRTIs.
Truss analysis using the stiffness method                                        T.Chhay   -467
Department of Civil Engineering                                                                          NPIC




!$>#> m:aRTIsbMElgénbMlas;TI nigkmøaMg
        (Displacement and force transformation matrices)
         edaysar truss pSMeLIgedayGgát;eRcIn eyIgnwg
begáItviFIsRmab;bMElgkmøaMgkñúgGgát; q nig bMlas;TI d
EdlkMNt;enAkñúgkUGredaentMbn;eGayeTACakUGredaen
skl. edIm,IPaBgayRsYl eyIgnwgBicarNakUGredaen
sklviC¢man x manTisedAeTAsþaM ehIy y manTisedA
eLIgelI. mMurvagG½kSskl x, y nigG½kStMbn; x' , y'
RtUv)ankMNt;eday θ x ehIy θ y dUcbgðajenAkñúgrUbTI
14-3. eyIgnwgeRbI kUsIunUsénmMuTaMgenHenAkñúgkarviPaK
m:aRTIsdUcteTA. eyIgtag λ x = cosθ x ehIy λ y = cosθ y . eKGackMNt;témøCaelxsRmab; λ x
nig λ y y:aggayedayeRbIkMuBüÚT½r enAeBleKkMNt; kUGredaen x, y éncugCit N nigcugq¶ay F rbs;
Ggát;rYcehIy. ]TahrN_ eKmanGgát; NF dUcbgðajenAkñúgrUbTI 14-4. enATIenH kUGredaenrbs; N
nig F KW (x N , y N ) nig (x F , y F ) erogKña . dUcenH
                                                *


                                  xF − x N               xF − xN
           λ x = cos θ x =                 =                                                   (14-5)
                                     L         (x F   − xN ) + (yF − y N )
                                                           2             2

                                  yF − yN                 yF − yN
           λ y = cos θ y =                =                                                    (14-6)
                                     L         (x F   − xN ) + (yF − yN )
                                                            2                2




*
  Kl;rbs;kUGredaenGacsßitenATINak¾)an eGayEtmanlkçN³gayRsYl. b:uEnþ CaTUeTA vaeRcInsßitenARtg;TItaMgNaEdl
kUGredaenrbs; node TaMgGs;viC¢man dUcbgðajenAkñúgrUbTI 14-4.
 karviPaK truss edayeRbIviFIPaBrwgRkaj                                                        T.Chhay   -468
mhaviTüal½ysMNg;sIuvil                                                   viTüasßanCatiBhubec©keTskm<úCa

sBaØanBVnþenAkñúgsmIkarTUeTATaMgenHnwgKitedaysV½yRbvtþisRmab;Ggát;EdlsßitenAkñúgkaRdg;NamYy
rbs;bøg; xy .




m:aRTIsbMElgbMlas;TI³ enAkñúgkUGredaenskl cugnImYy²rbs;Ggát;Gacman degree of freedom b¤
bMlas;TIÉkraCüBIr eBalKWtMN N man DN nig DN ¬rUbTI 14-5a nig 14-5b¦ ehIytMN N man
                                                    x       y


D F nig DF ¬rUbTI 14-5c nig14-5d¦. eyIgnwgBicarNabMlas;TITaMgenHdac;edayELkBIKñaedIm,I
      x            y


kMNt;bgÁúMbMlas;TIrbs;vatambeNþayGgát;. enAeBlcugq¶ayRtUv)anTb;edaysnøak; ehIycugCitmanbM
las;TItamkUGredaenskl DN ¬rUbTI 14-5a¦ bMlas;TI ¬kMhUcRTg;RTay¦ EdlRtUvKñatambeNþay
                                            x

Ggát;KW DN cosθ x *. dUcKña bMlas;TI DN nwgeFVIeGayGgát;pøas;TI DN cosθ y tambeNþayG½kS x'
               x                                        y            y


¬rUbTI 14-5b¦. T§iBlénbMlas;TIsklTaMgeFVIeGayGgát;pøas;TI.
           d N = D N x cos θ x + D N y cos θ y

tamrebobdUcKña bMlas;TIviC¢man DF nig DF erogKña EdlGnuvtþenARtg;cugq¶ay F cMENkÉcugCit
                                                x       y


RtUv)anTb;edaysnøak; ¬rUbTI 14-5c nig 14-5d¦ nwgeFVIeGayGgát;pøas;TI
           d F = D Fx cos θ x + D Fy cos θ y

edayeGay λ x = cosθ x nig λ y = cosθ y CakUsIunUsR)ab;Tis (direction cosine) sRmab;Ggát;
eyIg)an
           d N = DN x λ x + DN y λ y

           d F = DFx λ x + DFy λ y

EdleKGacsresrvaCaTRmg;m:aRTIs
                                  ⎡ DN x ⎤
                                  ⎢       ⎥
           ⎡ d N ⎤ ⎡λ x λ y 0 0 ⎤ ⎢ D N y ⎥
           ⎢d ⎥ = ⎢ 0 0 λ λ ⎥⎢ D ⎥                                                     (14-7)
           ⎣ F⎦ ⎣            x y⎦
                                  ⎢ x⎥
                                      F

                                  ⎢ D Fy ⎥
                                  ⎣       ⎦

*
    eKminKitBIbMEbMrYl θ x b¤ θ y edaysarvamantémøtUceBk.
Truss analysis using the stiffness method                                         T.Chhay   -469
Department of Civil Engineering                                                                   NPIC



b¤         d = TD                                                                       (14-8)
             ⎡λ x λ y 0 0 ⎤
Edl       T =⎢            ⎥                                                             (14-9)
             ⎣ 0 0 λx λ y ⎦
BIkarbMEbkxagelI T bMElgBIbMlas;TI D kñúgkUGredaenskl x, y TaMgbYneGayeTACabMlas;TI d kñúg
kUGredaentMbn; x' cMnYnBIr. dUcenH T Cam:aRTIsbMElgbMlas;TI.




m:aRTIsbMElgkmøaMg³ BicarNakarGnuvtþkmøaMg q eTAelIcugCitrbs;Ggát; cMENkcugq¶ayRtUv)anTb;
                                                 N

edaysnøak; ¬rUbTI 14-6a¦. enATIenH bgÁúMkmøaMgsklrbs; q N enARtg; N KW
          Q N x = q N cos x              Q N y = q N cos θ y

dUcKña RbsinebI q F RtUv)anGnuvtþeTAelIr)ar ¬rUbTI 14-6b¦ bgÁúMkmøaMgsklenARtg; F KW
          Q Fx = q F cos θ x             Q Fy = q F cos θ y

edayeRbIkUsIunUsR)ab;Tis λ x = cosθ x / λ y = cosθ y smIkarTaMgenHkøayCa
          QN x = q N λ x                 QN y = q N λ y

           Q Fx = q F λ x                Q Fy = q F λ y

EdleKGacsresrvaCaTRmg;m:aRTIsdUcxageRkam

 karviPaK truss edayeRbIviFIPaBrwgRkaj                                                 T.Chhay   -470
mhaviTüal½ysMNg;sIuvil                                                  viTüasßanCatiBhubec©keTskm<úCa
           ⎡Q N x ⎤ ⎡ λ x         0⎤
           ⎢Q ⎥ ⎢                  ⎥
           ⎢ N y ⎥ = ⎢λ y         0⎥ ⎡q N ⎤
                                λx ⎥ ⎢qF ⎥
                                                                                      (14-10)
           ⎢ QFx ⎥ ⎢ 0               ⎣ ⎦
           ⎢      ⎥ ⎢              ⎥
           ⎢ Q Fy ⎥ ⎢ 0
           ⎣      ⎦ ⎣           λy ⎥
                                   ⎦
b¤         Q =TTq                                                                     (14-11)
                  ⎡λ x     0⎤
                  ⎢λ       0⎥
Edl        TT    =⎢
                  ⎢0
                     y        ⎥
                           λx ⎥
                                                                                      (14-12)
                  ⎢           ⎥
                  ⎢0
                  ⎣        λy ⎥
                              ⎦
enAkñúgkrNIenH T T bMElgBIkmøaMg q EdlmanGMeBIenARtg;cugrbs;Ggát;kñúgkUGredaentMbn; x' eGayeTA
CakmøaMg Q EdlmanbgÁúMbYnkñúgkUGredaenskl x, y . tamkareRbobeFob m:aRTIsbMElgkmøaMgCa
m:aRTIs transpose énm:aRTIsbMElgbMlas;TI ¬smIkar 14-9¦.




!$>$> m:aRTIsPaBrwgRkajrbs;Ggát;kñúgkUGredaenskl
         (Member global stiffness matrix)
        eyIgnwgpþúMlT§plenAkñúgkfaxNÐxagelI ehIykMNt;m:aRTIsPaBrwgRkajsRmab;Ggát;EdlTak;
TgnwgbgÁúMkmøaMgskl Q nigbMlas;TIskl D rbs;Ggát;. RbsinebIeyIgCMnYssmIkar 14-8 ¬ d = TD ¦
eTAkñúgsmIkar 14-3 ¬ q = k ' d ¦ eyIgGackMNt;kmøaMg q rbs;Ggát;CaGnuKmn_énbMlas;TIskl D enA
Rtg;cMNuccugrbs;va eBalKW
                      q = k ' TD                                                      (14-13)
edayCMnYssmIkarenHeTAkñúgsmIkar 14-11 ¬ Q = T T q ¦ enaHeyIgnwgTTYl)anlT§plcugeRkay
                      Q = T T k ' TD
b¤                    Q = KD                                                          (14-14)

Truss analysis using the stiffness method                                        T.Chhay   -471
Department of Civil Engineering                                                                   NPIC



Edk              k = T T k 'T                                                 (14-15)

m:aRTIs k Cam:aRTIsPaBrwgRkajsRmab;Ggát;enAkñúgkUGredaenskl. edaysareKsÁal; T T / T nig k '
enaHeyIg)an
                       ⎡λ x        0⎤
                       ⎢λ          0 ⎥ AE ⎡ 1 − 1⎤ ⎡λ x λ y 0 0 ⎤
                     k=⎢              ⎥
                          y
                       ⎢0         λ x ⎥ L ⎢− 1 1 ⎥ ⎢ 0 0 λ x λ y ⎥
                                          ⎣      ⎦⎣              ⎦
                       ⎢              ⎥
                       ⎢0
                       ⎣          λy ⎥⎦
edayKNnaedaHRsaym:aRTIsxagelI eyIg)an
                                     Nx      Ny        Fx        Fy
                           ⎡ λ2 x           λxλ y     − λ2
                                                         x     − λxλ y ⎤ N x
                        AE ⎢                                            ⎥
                     k=    ⎢ λx λ y          λ2
                                              y      − λxλ y    − λ2 ⎥ N y
                                                                     y                  (14-16)
                         L ⎢
                           ⎢ − λx
                                  2
                                           − λxλ y     λ2
                                                        x       λ x λ y ⎥ Fx
                                                                        ⎥
                           ⎢− λ x λ y       − λ2     λxλ y          2 ⎥F
                                                                 λy ⎦ y
                           ⎣                   y

TItaMgrbs;tYnImYy³enAkñúgm:aRTIssIuemRTITMhM 4 × 4 tMNageGay degree of freedom sklnImYy²Edl
pSMCamYynwgcugCit N nigCamYynwgcugq¶ay F . vaRtUv)anbgðajedaynimitþsBaØénelxkUdEdlenAtam
CYredk nigCYrQr eBalKW N x , N y , Fx , Fy . enATIenH k CaTMnak;TMngrvagkmøaMg nigbMlas;TIsRmab;
Ggát;enAeBlEdlbgÁúMénkmøaMg nigbMlas;TIenAcugrbs;Ggát;sßitenAkñúgkUGredaenskl b¤G½kS x, y . dUc
enHtYnImYy²enAkñúgm:aRTIsCaemKuNT§iBlPaBrwgRkaj (stiffness influence coefficient) K ij Edl
bgðajbgÁúMkmøaMg x b¤ y enARtg; i EdlcaM)ac;edIm,IeFVIeGaymanbgÁúMbMlas;TIÉktþa x b¤ y enARtg; j . Ca
lT§pl CYrQrnImYy²rbs;m:aRTIstMNageGaybgÁúMkmøaMgbYnEdlekItmanenARtg;cugrbs;Ggát;enAeBl
cugGgát;rgbMlas;TIÉktþaEdlTak;TgnwgCYrQrebs;m:aRTIsenaH. ]TahrN_ bMlas;TIÉktþa DN = 1        x

nwgbegáItbgÁúMkmøaMgbYnenAelIGgát;EdlbgðajenAkñúgCYrQrTImYyrbs;m:aRTIs.

!$>%> ma:RTIsPaBrwgRkajsMrab; truss (Truss stiffness matrix)
        eRkayeBlbegáItm:aRTIsPaBrwgRkajsRmab;Ggát;enAkñúgkUGredaensklrYcehIy eKcaM)ac;pÁúMBUk
vabBa©ÚlKñatamlMdab;d¾RtwmRtUv dUcenHeKnwgTTYl)anm:aRTIsPaBrwgRkaj K sRmab; truss TaMgmUl. dM-
eNIrkarénkarpÁúMm:aRTIsGgát;TaMgenHGaRs½ynwgkarkMNt;GtþsBaØaNrbs;Ggát;enAkñúgm:aRTIsGgát;nImYy
². dUckarerobrab;enAkñúgkfaxNÐmun eKRtUvtMerobCYredk nigCYrQrrbs;m:aRTIsedayelxkUdbYn N x ,
 N y , Fx , Fy EdleRbIedIm,IkMNt;GtþsBaØaN degree of freedom sklBIrEdlGacekItmanenARtg;

cugnImYy²rbs;Ggát; ¬emIlsmIkar 14-16¦. m:aRTIsPaBrwgRkajsRmab;eRKOgbgÁúMnwgmanlMdab;esμInwg
 karviPaK truss edayeRbIviFIPaBrwgRkaj                                                 T.Chhay   -472
mhaviTüal½ysMNg;sIuvil                                                    viTüasßanCatiBhubec©keTskm<úCa

elxkUdx<s;bMputEdl)ankMNt;eTAelI truss edaysartMNageGaycMnYn degree of freedom srub
sRmab;eRKOgbgÁúM. enAeBleKpÁúMm:aRTIs k eKRtUvCMnYstYnImYy²enAkñúg k eTAkñúgCYredk nigCYrQrRtUvKña
rbs;m:aRTIsPaBrwgRkajsRmab;rcnasm<½n§ K . enAeBlGgát;BIr b¤Ggát;eRcIntP¢ab;KñaenARtg;tMNEtmYy
eKRtUvdak;tYénm:aRTIsrbs;Ggát; k xøHeTAkñúgTItaMgdEdlrbs;m:aRTIs K . eKRtUvbUkbBa©ÚlKñatamlkçN³
nBVnþnUvtYEdlsßitenAkñúgTItaMgdUcKña. eyIgnwgyl;BImUlehtuenH)anc,as; RbsinebIeyIgdwgfatYnImYy²
rbs;m:aRTIs k CaersIusþg;rbs;Ggát;Tb;Tl;nwgkmøaMgxageRkAEdlGnuvtþenARtg;cugrbs;va. tamviFIEbb
enH karbUkbBa©ÚlKñanUversIusþg;tamTis x nigTis y enAeBlbegáItm:aRTIs K kMNt;nUversIusþg;srubrbs;
tMNnImYy²EdlTb;Tl;nwgbMlas;TIÉktþatamTis x b¤tamTis y .
         ]TahrN_CaelxcMnYnBIrnwgbgðajBIviFIénkarpÁúMm:aRTIssRmab;Ggát;edIm,IbegáItCam:aRTIsPaBrwg
RkajsRmab;eRKOgbgÁúM. eTaHbIvadMeNIrkarmanlkçN³sμúKsμajsRmab;karKNnaedayédbnþic Etvaman
lkçN³gayRsYlCagsMrab;karbegáItkmμviFIenAelIkMuBüÚT½r.
]TahrN_ 14-1³ kMNt;m:aRTIsPaBrwgRkajsRmab; truss EdlmanGgát;BIrdUcbgðajenAkñúgrUbTI
14-7a. AE mantémøefr.




dMeNaHRsay³ tamkarGegát ②manbgÁúMbMlas;TIEdlCaGBaØatcMnYnBIr cMENkÉ ① nig③RtUv)anTb;
mineGaymanbMlas;TI. Cavi)ak eKRtUvkMNt;elxkUdeGaybgÁúMbMlas;TIenARtg;tMN ② dMbUgeK ehIy
bnþedaytMN ③ nig ① ¬rUbTI14-7b¦. eKalrbs;RbB½n§kUGredaensklGacsßitenAcMNucNak¾)an.
edIm,IPaBgayRsYl eyIgnwgeRCIserIstMN ② dUcbgðaj. eyIgGackMNt;elxerogeGayGgát;tam
rebobNak¾)an ehIyeKRtUvKUssBaØaRBYjtambeNÞayGgát;TaMgBIredIm,IeGaydwgcugCit nigcugq¶ay
bs;Ggát;nImYy². eKGacKNnakUsIunUsR)ab;Tis nigm:aRTIsPaBrwgRkajsRmab;Ggát;nImYy².
Truss analysis using the stiffness method                                          T.Chhay   -473
Department of Civil Engineering                                                              NPIC



Ggát;elx1³ edaysar ②CacugCit ehIy ③Cacugq¶ay enaHtamsmIkar14-5 nig14-6 eyIg)an
                  3−0                                   0−0
           λx =       =1                         λy =       =0
                   3                                     3
edayeRbIsmIkar 14-16 nigedayEcktYnImYy²CamYynwg L = 3m eyIg)an
                      1              2     3      4
                   ⎡ 0.333           0 − 0.333    0⎤ 1
                   ⎢                              0⎥ 2
           k1 = AE ⎢ 0               0    0        ⎥
                   ⎢− 0.333          0 0.333      0⎥ 3
                   ⎢                               ⎥
                   ⎣ 0               0    0       0⎦ 4

eyIgGacRtYtBinitükarKNnaedaycMNaMfa k1 Cam:aRTIssIuemRTI. cMNaMfa CYredk nigCYrQrenAkñúg
m:aRTIs k1 RtUv)ankMNt;eday degree of freedom x, y enAcugCit Edlbnþedaycugq¶ay eBalKW 1,
2, 3 nig 4 erogKña sRmab;Ggát;elx1 ¬rUbTI 14-7b¦. eKeFVIEbbenHedIm,IkMNt;tYsRmab;karpÁúMenAkñúg

m:aRTIs K .
Ggát;elx 2³ edaysar ②CacugCit ehIy ①Cacugq¶ay enaHeyIg)an
                  3−0                                   4−0
           λx =       = 0.6                      λy =       = 0.8
                   5                                     3
dUcenHsmIkar 14-16 CamYynwg L = 5m køayCa
                        1       2      5       6
                    ⎡ 0.072   0.096 − 0.072 − 0.096⎤ 1
                    ⎢         0.128 − 0.096 − 0.128⎥ 2
           k 2 = AE ⎢ 0.096                        ⎥
                    ⎢− 0.072 − 0.096 0.072   0.096 ⎥ 5
                    ⎢                              ⎥
                    ⎣− 0.096 − 0.128 0.096   0.128 ⎦ 6

enATIenH eKkMNt;CYredk nigCYrQrCa1, 2, 5 nig 6 edaysarelxTaMgenHtMNageGay degree of
freedom tamTis x nig y enARtg;cugCit nigcugq¶ayrbs;Ggát;elx 2 .

m:aRTIsPaBrwgRkajsRmab;rcnasm<½n§³ vaCam:aRTIsTMhM 6 × 6 edaysarvaman degree of freedom
sRmab; truss cMnYn 6 ¬rUbTI 14-7b¦. eKRtUvbUktYEdlRtUvKñaénm:aRTIsTaMgBIrxagelIedIm,IbegáItCa
m:aRTIsPaBrwgRkajsRmab;eRKOgbgÁúM. eKRbEhlCaRsYlemIlCagRbsinebIeKBnøatm:aRTIs k1 nig k 2
eGayeTACam:aRTIs 6 × 6 . enaHeK)an
           K = k1 + k 2




 karviPaK truss edayeRbIviFIPaBrwgRkaj                                            T.Chhay   -474
mhaviTüal½ysMNg;sIuvil                                                                viTüasßanCatiBhubec©keTskm<úCa
          1                 2     3         4    5    6             1     2       3   4      5      6
       ⎡ 0.333              0 − 0.333       0   0    0⎤ 1      ⎡ 0.072   0.096    0   0 − 0.072 − 0.096⎤ 1
       ⎢ 0                  0    0          0   0     ⎥
                                                     0⎥ 2      ⎢ 0.096   0.128    0   0 − 0.096 − 0.128⎥ 2
       ⎢                                                       ⎢                                       ⎥
K = AE ⎢− 0.333             0 0.333         0   0    0⎥ 3 + AE ⎢ 0         0      0   0    0       0 ⎥3
       ⎢                                              ⎥        ⎢                                       ⎥
       ⎢ 0                  0    0          0   0    0⎥ 4      ⎢ 0         0      0   0    0       0 ⎥4
       ⎢ 0                  0    0          0   0    0⎥ 5      ⎢− 0.072 − 0.096   0   0 0.072    0.096 ⎥ 5
       ⎢                                              ⎥        ⎢                                       ⎥
       ⎢ 0
       ⎣                    0    0          0   0    0⎥ 6
                                                      ⎦        ⎢− 0.096 − 0.128
                                                               ⎣                  0   0 0.096    0.128 ⎥ 6
                                                                                                       ⎦

       ⎡ 0.405   0.096 − 0.333                       0 − 0.072 − 0.096⎤
       ⎢ 0.096   0.128    0                          0 − 0.096 − 0.128⎥
       ⎢                                                              ⎥
K = AE ⎢ − 0.333   0    0.333                        0    0       0 ⎥
       ⎢                                                              ⎥
       ⎢ 0         0      0                          0    0       0 ⎥
       ⎢− 0.072 − 0.096   0                          0 0.072    0.096 ⎥
       ⎢                                                              ⎥
       ⎢− 0.096 − 0.128
       ⎣                  0                          0 0.096    0.128 ⎥
                                                                      ⎦
RbsinebIeKeFVIdMeNIrkarenHCamYynwgkMuBüÚT½r CaTUeTAeKcab;epþImCamYynwgm:aRTIs K EdlmanFatuTaMg
Gs;esμIsUnü bnÞab;mkFatuénm:aRTIsPaBrwgRkajsklsRmab;Ggát;Edl)anKNnarYcehIyRtUv)anCMnYs
edaypÞal;eTAkñúgTItaMgFatuEdlRtUvKñaénm:aRTIs K . kareFVIEbbenHvaRbesIrCagkarbegáItm:aRTIsPaBrwg
RkajsRmab;Ggát; rUcehIyrkSavaTuk bnÞab;mkeTIbpÁúMva.

]TahrN_ 14-2³ kMNt;m:aRTIsPaBrwgRkajsRmab; truss EdlmanGgát;BIrdUcbgðajenAkñúgrUbTI
14-8a. AE mantémøefr.




dMeNaHRsay³ eTaHbICa truss Carcnasm<½n§minkMNt;edaysþaTicdWeRkTImYyk¾eday Etvanwgminbgðaj
BIPaBlM)akkñúgkarTTYl)anm:aRTIsPaBrwgRkajsRmab;rcnasm<½n§eT. eKkMNt;elxerogeGaytMN nig
Truss analysis using the stiffness method                                                      T.Chhay   -475
Department of Civil Engineering                                                              NPIC



Ggát;nImYy² ehIyeKbgðajcugCit nigcugq¶ayedayRBYjtambeNþayGgát;. dUcbgðajenAkñúgrUbTI 14-
8b dMbUgeKkMNt;elxerogkUdeGaybMlas;TIEdlminRtUv)anTb;. eKman degree of freedom cMnUn 8
dUcenH K RtUvCam:aRTIsTMhM 8 × 8 . edIm,IrkSaeGaykUGredaenrbs;tMNTaMgGs;viC¢man eKRtUveRCIserIs
eKalrbs;kUGredaensklenARtg; ①. eyIgnwgGnuvtþsmIkar 14-5, 14-6 nig 14-16 eTAelIGgát;
nImYy².
Ggát;elx 1³ enATIenH L = 10m eyIg)an
                10 − 0                                         0−0
           λx =        =1                               λy =       =0
                 10                                             10
                      1           2   6        5
                   ⎡ 0.1          0 − 0.1      0⎤ 1
                   ⎢                           0⎥ 2
           k1 = AE ⎢ 0            0   0          ⎥
                   ⎢− 0.1         0   1        0⎥ 6
                   ⎢                             ⎥
                   ⎣ 0            0   0        0⎦ 5

Ggát;elx 2³ enATIenH L = 10               2m   dUcenH
                  10 − 0                                       10 − 0
           λx =             = 0.707                     λy =            = 0.707
                  10 2                                         10 2
                         1       2      7      8
                    ⎡ 0.035   0.035 − 0.035 − 0.035⎤ 1
                    ⎢ 0.035   0.035 − 0.035 − 0.035⎥ 2
           k 2 = AE ⎢                              ⎥
                    ⎢− 0.035 − 0.035 0.035   0.035 ⎥ 7
                    ⎢                              ⎥
                    ⎣− 0.035 − 0.035 0.035   0.035 ⎦ 8

Ggát;elx 3³ enATIenH L = 10m dUcenH
                 0−0                                           10 − 0
           λx =        =0                               λy =          =1
                  10                                            10
                     1    2              3   4
                    ⎡0    0              0   0 ⎤1
                    ⎢0 0.1               0 − 0.1⎥ 2
           k 3 = AE ⎢                           ⎥
                    ⎢0    0              0   0 ⎥3
                    ⎢                           ⎥
                    ⎣0 − 0.1             0 0.1 ⎦ 4

Ggát;elx 4³ enATIenH L = 10m eyIg)an
                 10 − 0                                        0−0
           λx =         =1                              λy =       =0
                  10                                            10
                        3         4  7         8
                     ⎡ 0.1        0 − 0.1      0⎤ 3
                     ⎢                         0⎥ 4
           k 4 = AE ⎢ 0           0   0          ⎥
                     ⎢− 0.1       0   1        0⎥ 7
                     ⎢                           ⎥
                     ⎣ 0          0   0        0⎦ 8

 karviPaK truss edayeRbIviFIPaBrwgRkaj                                            T.Chhay   -476
mhaviTüal½ysMNg;sIuvil                                                               viTüasßanCatiBhubec©keTskm<úCa

Ggát;elx 5³ enATIenH L = 10                 2m   dUcenH
                   10 − 0                                        0 − 10
           λx =              = 0.707                      λy =            = −0.707
                   10 2                                          10 2
                         3      4        6    5
                    ⎡ 0.035 − 0.035 − 0.035 0.035 ⎤ 3
                    ⎢                0.035 − 0.035⎥ 4
           k 5 = AE ⎢− 0.035 0.035                ⎥
                    ⎢− 0.035 0.035   0.035 − 0.035⎥ 6
                    ⎢                             ⎥
                    ⎣ 0.035 − 0.035 − 0.035 0.035 ⎦ 5
Ggát;elx 3³ enATIenH L = 10m dUcenH
                 0−0                                             10 − 0
           λx =        =0                                 λy =          =1
                  10                                              10
                      6   5             7  8
                    ⎡0    0             0   0 ⎤6
                    ⎢0 0.1              0 − 0.1⎥ 5
           k 6 = AE ⎢                          ⎥
                    ⎢0    0             0   0 ⎥7
                    ⎢                          ⎥
                    ⎣0 − 0.1            0 0.1 ⎦ 8

m:aRTIsPaBrwgRkajsRmab;rcnasm<½n§³ eKGacpÁúMm:aRTIsTaMg 6 edIm,IbegáItm:aRTIsTMhM 8 × 8 edaykarbUk
bBa©ÚlFatuEdlRtUvKña. ]TahrN_ edaysar (k11 )1 = AE (0.1) / (k11 )2 = AE (0.035) / (k11 )3 =
(k11 )4 = (k11 )5 = (k11 )6 = 0 enaH K11 = AE (0.1 + 0.035) = AE (0.135) . dUcenHlT§plcugeRkayKW
                1          3   2  4      5      6        7      8
       ⎡       0.135       0 0.0350      0    − 0.1 − 0.035 − 0.035⎤ 1
       ⎢       0.035       0    − 0.1
                             0.135       0      0    − 0.035 − 0.035⎥ 2
       ⎢                                                            ⎥
       ⎢         0       0.135 − 0.035 0.035 − 0.035 − 0.1
                               0                                0 ⎥3
       ⎢                                                            ⎥
K = AE ⎢ 0              − 0.035 0.135 − 0.035 0.035
                             − 0.1                      0       0 ⎥4
       ⎢ 0         0     0.035 − 0.035 0.135 − 0.035    0     − 0.1 ⎥ 5
       ⎢                                                            ⎥
       ⎢ − 0.1     0    − 0.035 0.035 − 0.035 0.135     0       0 ⎥6
       ⎢− 0.035 − 0.035 − 0.1     0      0      0     0.135   0.035 ⎥ 7
       ⎢                                                            ⎥
       ⎢− 0.035 − 0.035
       ⎣                   0      0    − 0.1    0     0.135   0.135 ⎥ 8
                                                                    ⎦



!$>^> karGnuvtþénviFIPaBrwgRkajsRmab;karviPaK truss
(Application of the stiffness method for truss analysis)
     eRkayeBlbegáItm:aRTIsPaBrwgRkajsRmab;eRKOgbgÁúMrYcehIy eKGaceFVIeGaybgÁúMkmøaMgskl
Q EdlmanGMeBIenAelI truss manTMnak;TMngeTAnwgbMlas;TIskl D rbs;vaedayeRbI
                      Q = KD                                                                       (14-17)




Truss analysis using the stiffness method                                                     T.Chhay   -477
Department of Civil Engineering                                                              NPIC



eKGacsMKal;smIkarenHCasmIkarPaBrwgRkajsRmab;rcnasm<½n§ (structure stiffness equation).
edaysareyIgEtgEtkMNt;elxkUdtUcbMputedIm,IsmÁal; degree of freedom EdlminRtUv)anTb; dUcenH
vaGnuBaØateGayeyIgGacbMEbksmIkarenHkñúgTRmg;dUcxageRkam ³  *


                     ⎡Qk ⎤ ⎡ K11 K12 ⎤ ⎡ Du ⎤
                     ⎢Q ⎥ = ⎢ K      ⎥⎢ ⎥                                          (14-18)
                     ⎣ u ⎦ ⎣ 21 K 22 ⎦ ⎣ Dk ⎦
Edl               bnÞúkxageRkA nigbMlas;TIEdleKsÁal;. enATIenH bnÞúkmanGMeBIenAelI truss CaEpñk
          Qk , Dk =

                  mYyéncMeNaT ehIyCaTUeTAbMlas;TIesμIsUnüedaysarTMrRtUv)anTb; dUcCaTMrsnøak;
                  b¤TMrkl;.
      Qu , Du = bnÞúk nigbMlas;TIEdlCaGBaØat. enATIenH bnÞúkCakmøaMgRbtikmμTMrEdleKminsÁal;

                  ehIybMlas;TIKWsßitenARtg;tMNEdlminRtUv)anTb;tamTisNamYyeT.
       K = m:aRTIsPaBrwgRkajsRmab;rcnasm<½n§ EdlRtUv)anbMEbkedIm,IeGaycuHsRmugCamYynwg

           karbMEbkrbs; Q nig D .
edayBnøatsmIkar 14-18 eyIg)an
                  Qk = K11 Du + K12 Dk                                             (14-19)
                  Qu = K 21 Du + K 22 Dk                                           (14-20)
CaTUeTA Dk = 0 edaysarTMrminmanbMlas;TI. RbsinebIvaEbbenHEmn enaHsmIkar 14-19 køayCa
                  Qk = K11 Du
edaysarFatuenAkñúgm:aRTIs K11 CaersIusþg;srubenARtg;tMN truss edIm,ITb;Tl;bMlas;TIÉktþatamTI x
b¤ y enaHsmIkarxagelICakarRbmUlpþúMnUvsmIkarlMnwgkmøaMgEdlGnuvtþeTAelItMNEdlbnÞúkxageRkA
esμIsUnü b¤mantémøEdlsÁal; (Qk ) . edayedaHRsayrk Du eyIg)an
                     Du = [K11 ]−1 Qk                                              (14-21)
BIsmIkarenH eyIgGacTTYl)andMeNaHRsayedaypÞal;sRmab;bMlas;TIEdlCaGBaØatTaMgGs; bnÞab;mk
edayeRbIsmIkar 14-20 CamYynwg Dk = 0 eyIg)an
                     Qu = K 21 Du                                                  (14-22)
BIsmIkarxagelI eyIgGackMNt;kmøaMgRbtikmμTMr. eKGackMNt;kmøaMgkñúgrbs;Ggát;edayeRbIsmIkar
14-13 eBalKW

                     q = k ' TD
edayBnøatsmIkarenH eyIg)an

*
    eyIgnwg)aneXIjBIviFIbMEbkenHenAkñúg]TahrN_xageRkam.
 karviPaK truss edayeRbIviFIPaBrwgRkaj                                            T.Chhay   -478
mhaviTüal½ysMNg;sIuvil                                                      viTüasßanCatiBhubec©keTskm<úCa
                                                                 ⎡ DN x ⎤
                                                                 ⎢      ⎥
                      ⎡q N ⎤ AE ⎡ 1 − 1⎤ ⎡λ x λ y 0         0 ⎤ ⎢ D Ny ⎥
                      ⎢ q ⎥ = L ⎢− 1 1 ⎥ ⎢ 0 0 λ           λ y ⎥ ⎢ DFx ⎥
                      ⎣ F⎦      ⎣      ⎦⎣          x           ⎦⎢       ⎥
                                                                 ⎢ DFy ⎥
                                                                 ⎣      ⎦
edaysar q N = −q F edIm,IsßanPaBlMnwg dUcenHeKRtUvkarkMNt;EtkmøaMgmYyb:ueNÑaHkñúgcMeNamkmøaMg
TaMgBIr. enATIenH eyIgnwgkMNt; q F kmøaMgEdlGnuvtþkmøaMgTajeTAelIGgát; ¬rUbTI 14-6b¦.
                                                     ⎡ DN x ⎤
                                                     ⎢D ⎥
                      qF =
                               AE
                                L
                                    [
                                  − λx − λ y λx      ]
                                                  λy ⎢ y ⎥
                                                        N
                                                     ⎢ DFx ⎥
                                                                                          (14-23)
                                                     ⎢      ⎥
                                                     ⎢ D Fy ⎥
                                                     ⎣      ⎦
RbsinebIlT§plEdl)anBIkarKNnamantémøGviC¢man enaHGgát;rgkarsgát;.

dMeNIrkarkñúgkarviPaK (Procedure for analysis)
       xageRkamCaCMhanEdlpþl;nUvmeFüa)aysRmab;kMNt;bMlas;TI nigkmøaMgRbtikmμTMrEdlCa
GBaØatsRmab; truss edayeRbIviFIPaBrwgRkaj.
kareFVIkMNt;sMKal;³
          begáItRbB½n§kUGredaenskl x, y . CaTUeTAeKalrbs;vasßitenARtg;tMNNaEdleFVIeGay
          kUGredaensRmab;tMNdéTeTotviC¢man.
          kMNt;elxerogeGaytMN nigGgát;nImYy² ehIykMNt;cugCit nigcugq¶ayrbs;Ggát;nImYy²
          edayeRbITisedArbs;sBaØaRBYj Edlk,alRBYjeq<aHeTArkcugq¶ay.
          kMNt;elxkUdBIrenARtg;tMNnImYy² edayeRbIelxtUcbMputsRmab;sMKal; degree of freedom
          EdlminmanrgkarTb; cMENkelxFMbMputsRmab;sMKal; degree of freedom EdlmankarTb;.
          begáIt Dk nig Qk .
m:aRTIsPaBrwgRkajsRmab;eRKOgbgÁúM³
          sRmab;Ggát;nImYy² kMNt; λ x nig λ y ehIykMNt;m:aRTIsPaBrwgRkajsRmab;Ggát;edayeRbI
          smIkar 14-16.
          pÁúMm:aRTIsTaMgenHedIm,IbegáItm:aRTIsPaBrwgRkajsRmab; truss TaMgmUl dUckarBnül;enAkñúg
          kfaxNÐ 14-5. edaykarRtYtBinitükarKNnaedayEpñk m:aRTIsPaBrwgRkajsRmab;Ggát; nig
          m:aRTIsPaBrwgRkajsRmab;rcnasm<½n§RtUvEtCam:aRTIssIuemRTI.
bMlas;TI nigbnÞúk³
Truss analysis using the stiffness method                                            T.Chhay   -479
Department of Civil Engineering                                                             NPIC



          bMEbkm:aRTIsPaBrwgRkajsRmab;rcnasm<½n§ dUcbgðajenAkñúgsmIkar 14-18.
          kMNt;bMlas;TIrbs;tMNEdlCaGBaØat Du edayeRbIsmIkar 14-21 kmøaMgRbtikmμTMr Qu eday
          eRbIsmIkar 14-22 ehIykmøaMgkñúgrbs;Ggát;nImYy² q F edayeRbIsmIkar 14-23.

]TahrN_ 14-3³ kMNt;kmøaMgkñúgrbs;Ggát;én truss EdlmanGgát;BIrdUcbgðajenAkñúgrUbTI 14-9a.
AE   mantémøefr.




dMeNaHRsay³
kareFVIkMNt;smÁal;³ eKal x, y nigkarkMNt;elxerogrbs;tMN nigGgát;RtUv)anbgðajenAkñúgrUbTI
14-9b. dUcKña cugCit nigcugq¶ayRtUv)anbgðajkMNt;edaysBaØaRBYj ehIyeKeRbIelxkUdenARtg;tMN
nImYy². tamkarGegáteyIgeXIjfabMlas;TI D3 = D4 = D5 = D6 = 0 . ehIybnÞúkxageRkAEdl
eyIgsÁal;KW Q1 = 0, Q2 = −2kN . dUcenH
                ⎡0 ⎤ 3
                ⎢0 ⎥ 4
                                              ⎡ 0 ⎤1
           Dk = ⎢ ⎥                      Qk = ⎢ ⎥
                ⎢0 ⎥ 5                        ⎣ − 2⎦ 2
                ⎢ ⎥
                ⎣0 ⎦ 6
m:aRTIsPaBrwgRkajsRmab;rcnasm<½n§³ edayeRbIkareFVIkMNt;smÁal;dUcKña eyIgGacbegáItm:aRTIsPaBrwg
RkajsRmab;rcnasm<½n§dUcbgðajenAkñúg]TahrN_ 14-1.
bMlas;TI nigbnÞúk³ edaysresrsmIkar 14-17 ¬ Q = KD ¦ sRmab; truss eyIg)an

 karviPaK truss edayeRbIviFIPaBrwgRkaj                                           T.Chhay   -480
mhaviTüal½ysMNg;sIuvil                                                             viTüasßanCatiBhubec©keTskm<úCa
⎡0 ⎤     ⎡ 0.405   0.096 − 0.333                       0 − 0.072 − 0.096⎤ ⎡ D1 ⎤
⎢ − 2⎥   ⎢ 0.096   0.128    0                          0 − 0.096 − 0.128⎥ ⎢ D2 ⎥
⎢ ⎥      ⎢                                                              ⎥⎢ ⎥
⎢ Q3 ⎥   ⎢ − 0.333   0    0.333                        0    0       0 ⎥⎢ 0 ⎥
⎢ ⎥ = AE ⎢                                                              ⎥⎢ ⎥                     (1)
⎢ Q4 ⎥   ⎢ 0         0      0                          0    0       0 ⎥⎢ 0 ⎥
⎢ Q5 ⎥   ⎢− 0.072 − 0.096   0                          0 0.072    0.096 ⎥ ⎢ 0 ⎥
⎢ ⎥      ⎢                                                              ⎥⎢ ⎥
⎢Q6 ⎥
⎣ ⎦      ⎢− 0.096 − 0.128
         ⎣                  0                          0 0.096    0.128 ⎥ ⎢ 0 ⎥
                                                                        ⎦⎣ ⎦
BIsmIkarenH eyIgGackMNt; K11 dUcenHeyIgGackMNt; Du . eyIgeXIjfaplKuNm:aRTIs ¬dUc
smIkar 14-19¦ eyIg)an
           ⎡0 ⎤       ⎡0.405 0.096⎤ ⎡ D1 ⎤ ⎡0⎤
           ⎢− 2⎥ = AE ⎢0.096 0.128⎥ ⎢ D ⎥ + ⎢0⎥
           ⎣ ⎦        ⎣           ⎦⎣ 2 ⎦ ⎣ ⎦
enATIenH eyIgGacedaHRsayy:agRsYledayBnøatedaypÞal;
           0 = AE (0.405 D1 + 0.096 D2 )

           − 2 = AE (0.096 D1 + 0.128 D2 )
tamrUbviTüa smIkarTaMgenHtMNageGay ∑ Fx = 0 nig ∑ Fy = 0 EdlGnuvtþenARtg;tMN ②. eday
edaHRsay eyIg)an
                   4.505                           − 19.003
           D1 =                             D2 =
                    AE                                AE
tamkarGegátrUbTI 14-9b eKrMBwgfatMN ②nwgpøas;TIeTAsþaM nigcuHeRkamdUcbgðajedaysBaØabUk nig
sBaØadkéncemøIyenH
edayeRbIlT§plTaMgenH eKGacTTYl)ankmøaMgRbtikmμTMrBIsmIkar (1) EdlRtUv)ansresrkñúgTRmg;én
smIkar 14-20 ¬b¤smIkar 14-22¦ Ca
           ⎡Q3 ⎤      ⎡ − 0.333   0 ⎤                  ⎡0 ⎤
           ⎢Q ⎥       ⎢ 0             ⎥
                                  0 ⎥ 1 ⎡ 4.505 ⎤ ⎢0⎥
           ⎢ 4 ⎥ = AE ⎢                               +⎢ ⎥
           ⎢Q5 ⎥      ⎢− 0.072 − 0.096⎥ AE ⎢− 19.003⎥ ⎢0⎥
                                           ⎣        ⎦
           ⎢ ⎥        ⎢               ⎥                ⎢ ⎥
           ⎣Q6 ⎦      ⎣− 0.096 − 0.128⎦                ⎣0 ⎦
edayBnøat nigedaHRsaykmøaMgRbtikmμ
           Q3 = −0.333(4.505) = −1.5kN

           Q4 = 0
           Q5 = −0.072(4.505) − 0.096(− 19.003) = 1.5kN

           Q6 = −0.096(4.505) − 0.128(− 19.003) = 2.0kN
eKGacKNnakmøaMgenAkñúgGgát;nImYy²BIsmIkar 14-23. edayeRbITinñn½ysRmab; λ x nig λ y enAkñúg
smIkar 14-1 eyIg)an
Truss analysis using the stiffness method                                                   T.Chhay   -481
Department of Civil Engineering                                                           NPIC



Ggát;elx ! ³ λ x = 1,         λ y = 0, L = 3m
                                   ⎡ 4.505 ⎤ 1
                                   ⎢       ⎥
                AE 1 2 3 4 1 ⎢− 19.003⎥ 2
           q1 =
                  3 [− 1 0 1 0] AE ⎢ 0 ⎥ 3
                                   ⎢       ⎥
                                   ⎣ 0 ⎦4
              = [− 4.505] = −1.5kN
                1
                3
Ggát;elx @ ³ λ x = 0.6,           λ y = 0.8, L = 5m
                                               ⎡ 4.505 ⎤ 1
                 AE 1       2     5     6 1 ⎢− 19.003⎥ 2
                                               ⎢       ⎥
           q2 =
                  5 [− 0.6 − 0.8 0.6 0.8] AE ⎢ 0 ⎥ 5
                                               ⎢       ⎥
                                               ⎣ 0 ⎦6
              = [− 0.6(4.505) − 0.8(− 19.003)] = 2.5kN
                1
                5
Cak;EsþgeKGacepÞógpÞat;cemøIyTaMgenHedaysmIkarlMnwgEdlGnuvtþenARtg;tMN ②.

]TahrN_ 14-4³ kMNt;kmøaMgRbtikmμTMr nigkmøaMgkñúgrbs;Ggát;elx@ én truss dUcbgðajenAkñúgrUbTI
14-10a. AE mantémøefr.




dMeNaHRsay³
kareFVIkMNt;smÁal;³tMN nigGgát;RtUv)ankMNt;elxerog ehIyeKalrbs;G½kS x, y RtUv)anbegáItenA
Rtg;tMN ① ¬rUbTI 14-10b¦. ehIysBaØaRBYjRtUv)aneKeRbIedIm,IbgðajcugCit nigcugq¶ayrbs;Ggát;
nImYy². edayeRbIelxkUd EdlelxtUcbMputtMNageGay degree of freedom EdlmanrgkarTb; ¬rUb
TI 14-16b¦ eyIg)an

 karviPaK truss edayeRbIviFIPaBrwgRkaj                                         T.Chhay   -482
mhaviTüal½ysMNg;sIuvil                                                   viTüasßanCatiBhubec©keTskm<úCa
                                                  ⎡ 0 ⎤1
                                                  ⎢ 0 ⎥2
                             ⎡0 ⎤ 6               ⎢ ⎥
                       D k = ⎢0 ⎥ 7
                             ⎢ ⎥             Qk = ⎢ 2 ⎥ 3
                                                  ⎢ ⎥
                             ⎢0 ⎥ 8
                             ⎣ ⎦                  ⎢ − 4⎥ 4
                                                  ⎢ 0 ⎥5
                                                  ⎣ ⎦
 m:aRTIsPaBrwgRkajsRmab;rcnasm<½n§³ m:aRTIsenHRtUv)ankMNt;enAkñúg]TahrN_ 14-2 edayeRbIkar
 eFVIkMNt;smÁal;dUcKñanwgkarbgðajenAkñúg]TahrN_ 14-10b.
 bMlas;TI nigbnÞúk³ sRmab;cMeNaTenH Q = KD KW
⎡0⎤        ⎡ 0.135   0.035     0      0      0    − 0.1 − 0.035 − 0.035⎤ ⎡ D1 ⎤
⎢0⎥        ⎢ 0.035   0.135     0    − 0 .1   0      0    − 0.035 − 0.035⎥ ⎢ D2 ⎥
⎢ ⎥        ⎢                                                            ⎥⎢ ⎥
⎢ 2⎥       ⎢ 0         0     0.135 − 0.035 0.035 − 0.035 − 0.1      0 ⎥ ⎢ D3 ⎥
⎢ ⎥        ⎢                                                            ⎥⎢ ⎥
⎢− 4⎥ = AE ⎢ 0       − 0.1 − 0.035 0.135 − 0.035 0.035      0       0 ⎥ ⎢ D4 ⎥
                                                                                 (1)
⎢0⎥        ⎢ 0         0     0.035 − 0.035 0.135 − 0.035    0     − 0.1 ⎥ ⎢ D5 ⎥
⎢ ⎥        ⎢                                                            ⎥⎢ ⎥
⎢Q6 ⎥      ⎢ − 0 .1    0    − 0.035 0.035 − 0.035 0.135     0       0 ⎥⎢ 0 ⎥
⎢Q ⎥       ⎢− 0.035 − 0.035 − 0.1     0      0      0     0.135   0.035 ⎥ ⎢ 0 ⎥
⎢ 7⎥       ⎢                                                            ⎥⎢ ⎥
⎢ Q8 ⎥
⎣ ⎦        ⎢− 0.035 − 0.035
           ⎣                   0      0    − 0 .1   0     0.035   0.135 ⎥ ⎢ 0 ⎥
                                                                        ⎦⎣ ⎦


 edayeFVIplKuNdUckarsresrsmIkar 14-18 edIm,IedaHRsaybMlas;TI eyIg)an
 ⎡0 ⎤       ⎡0.135 0.035    0      0      0 ⎤ ⎡ D1 ⎤ ⎡0⎤
 ⎢0 ⎥
 ⎢ ⎥
            ⎢0.035 0.135
            ⎢               0    − 0 .1   0 ⎥ ⎢ D2 ⎥ ⎢0 ⎥
                                              ⎥⎢ ⎥ ⎢ ⎥
 ⎢ 2 ⎥ = AE ⎢ 0      0    0.135 − 0.035 0.035 ⎥ ⎢ D3 ⎥ + ⎢0⎥
 ⎢ ⎥        ⎢                                 ⎥⎢ ⎥ ⎢ ⎥
 ⎢ − 4⎥     ⎢ 0    − 0.1 − 0.035 0.135 − 0.035⎥ ⎢ D4 ⎥ ⎢0⎥
 ⎢0 ⎥
 ⎣ ⎦        ⎢ 0
            ⎣        0    0.035 − 0.035 0.135 ⎥ ⎢ D5 ⎥ ⎢0⎥
                                              ⎦⎣ ⎦ ⎣ ⎦
 edayBnøat nigedayedaHRsaysmIkarsRmab;bMlas;TI eyIg)an
 ⎡ D1 ⎤     ⎡ 17.94 ⎤
 ⎢D ⎥       ⎢− 69.20⎥
 ⎢ 2⎥     1 ⎢         ⎥
 ⎢ D3 ⎥ =   ⎢ − 2.06 ⎥
 ⎢ ⎥ AE ⎢             ⎥
 ⎢ D4 ⎥     ⎢ − 87.14 ⎥
 ⎢ D5 ⎥
 ⎣ ⎦        ⎢− 22.06⎥
            ⎣         ⎦
 edaybegáItsmIkar 14-20 BIsmIkar (1) EdleRbIlT§plEdl)anKNna eyIg)an
                                                                ⎡ 17.94 ⎤
                                                                ⎢ − 69.20⎥ 0
 ⎡Q6 ⎤     ⎡ − 0.1     0    − 0.035 0.035 − 0.035⎤
                                                                          ⎥ ⎡ ⎤
 ⎢Q ⎥ = AE ⎢− 0.035 − 0.035 − 0.1                             1 ⎢
 ⎢ 7⎥      ⎢                          0      0 ⎥ ⎥
                                                                ⎢ − 2.06 ⎥ + ⎢0⎥
                                                             AE ⎢         ⎥ ⎢ ⎥
 ⎢ ⎥
 ⎣Q8 ⎦     ⎢− 0.035 − 0.035
           ⎣                   0      0    − 0.1 ⎥
                                                 ⎦              ⎢ − 87.14 ⎥ ⎢0⎥
                                                                             ⎣ ⎦
                                                                ⎢− 22.06⎥
                                                                ⎣         ⎦
 edayBnøat nigKNnakmøaMgRbtikmμTMr eyIg)an
 Truss analysis using the stiffness method                                         T.Chhay   -483
Department of Civil Engineering                                                             NPIC



          Q6 = −4.0kN

          Q7 = 2.0kN

          Q8 = 4.0kN
sBaØadksRmab; Q6 bgðajfakmøaMgRbtikmμrbs;TMrkl;eFVIGMeBIkñúgTis x GviC¢man. eKGackMNt;kmøaMg
enAkñúgGgát;elx@ BIsmIkar 14-23 EdlBIsmIkar 14-2 λ x = 0.707, λ y = 0.707, L = 10 2m
dUcenH
                                                               ⎡ 17.94 ⎤
                                                               ⎢− 69.20⎥
                     q2 =
                           AE
                               [− 0.707 − 0.707 0.707 0.707] 1 ⎢       ⎥
                          10 2                              AE ⎢ 0 ⎥
                                                               ⎢       ⎥
                                                               ⎣ 0 ⎦

                          = 2.56kN


]TahrN_ 14-5³ kMNt;kmøaMgkñúgrbs;Ggát;elx@ énrcnasm<½n§dUcbgðajenAkñúgrUbTI 14-11a. Rb
sinebIenARtg;tMN① mansMrut 25mm . yk AE = 8(103 )kN .




dMeNaHRsay³
kareFVIkMNt;smÁal;³edIm,IPaBgayRsYl eKRtUvbegáIteKalrbs;kUGredaensklenARtg;tMN ③ dUc
bgðajenAkñúgrUbTI 14-11b ehIytamFmμta eKeRbIelxkUdtUcCageKedIm,ItMNageGay degree of
freedom EdlminmankarTb;. dUcenH
     ⎡ 0 ⎤3
     ⎢− 0.025⎥ 4
     ⎢       ⎥
     ⎢ 0 ⎥5                                   ⎡0 ⎤ 1
Dk = ⎢       ⎥                           Qk = ⎢ ⎥
     ⎢ 0 ⎥6                                   ⎣0 ⎦ 2
     ⎢ 0 ⎥7
     ⎢       ⎥
     ⎢ 0 ⎥8
     ⎣       ⎦
 karviPaK truss edayeRbIviFIPaBrwgRkaj                                           T.Chhay   -484
mhaviTüal½ysMNg;sIuvil                                                          viTüasßanCatiBhubec©keTskm<úCa

m:aRTIsPaBrwgRkajsRmab;rcnasm<½n§³ edayeRbIsmIkar 14-16 eyIg)an
Ggát;elx !³ λ x = 0 / λ y = 1 / L = 3m dUcenH
                     3    4                 1       2
                   ⎡0    0                  0       0⎤3
                   ⎢0 0.333                 0 − 0.333⎥ 4
           k1 = AE ⎢                                 ⎥
                   ⎢0    0                  0    0 ⎥1
                   ⎢                                 ⎥
                   ⎣0 − 0.333               0 0.333 ⎦ 2
Ggát;elx @³ λ x = −0.8,             λ y = −0.6, L = 5m           dUcenH
                         1      2        5       6
                    ⎡ 0.128    0.096 − 0.128 − 0.096⎤ 1
                    ⎢ 0.096    0.072 − 0.096 − 0.072⎥ 2
           k 2 = AE ⎢                               ⎥
                    ⎢ − 0.128 − 0.096 0.128   0.096 ⎥ 5
                    ⎢                               ⎥
                    ⎣− 0.096 − 0.072 0.096    0.072 ⎦ 6

Ggát;elx #³ λ x = 1,          λ y = 0, L = 4m           dUcenH
                        7            8    1         2
                    ⎡ 0.25           0 − 0.25       0⎤ 7
                    ⎢                               0⎥ 8
           k 3 = AE ⎢ 0              0   0            ⎥
                    ⎢− 0.25          0 0.25         0⎥ 1
                    ⎢                                 ⎥
                    ⎣ 0              0   0          0⎦ 2

edaypÁúMm:aRTIsTaMgenH m:aRTIsPaBrwgRkajsRmab;rcnasm<½n§køayCa
                   1      2                     3       4    5        6     7    8
              ⎡ 0.378    0.096                  0       0 − 0.128 − 0.096 − 0.25 0⎤ 1
              ⎢ 0.096    0.405                  0 − 0.333 − 0.096 − 0.072   0    0⎥ 2
              ⎢                                                                   ⎥
              ⎢ 0          0                    0    0       0       0      0    0⎥ 3
              ⎢                                                                   ⎥
           K =⎢ 0       − 0.333                 0 0.333      0       0      0    0⎥ 4
              ⎢ − 0.128 − 0.096                 0    0     0.128   0.096    0    0⎥ 5
              ⎢                                                                   ⎥
              ⎢− 0.096 0.072                    0    0     0.096   0.072    0    0⎥ 6
              ⎢ − 0.25     0                    0    0       0       0     0.25 0⎥ 7
              ⎢                                                                   ⎥
              ⎢ 0
              ⎣            0                    0    0       0       0      0    0⎥ 8
                                                                                  ⎦
bMlas;TI nigbnÞúk³ enATIenH Q = KD eyIg)an




Truss analysis using the stiffness method                                                T.Chhay   -485
Department of Civil Engineering                                                                 NPIC


⎡0⎤        ⎡ 0.378    0.096              0     0     − 0.128 − 0.096 − 0.25 0⎤ ⎡ D1 ⎤
⎢0⎥        ⎢ 0.096    0.405              0   − 0.333 − 0.096 − 0.072   0    0 ⎥ ⎢ D2 ⎥
⎢ ⎥        ⎢                                                                  ⎥⎢       ⎥
⎢Q3 ⎥      ⎢ 0          0                0      0       0       0      0    0⎥ ⎢ 0 ⎥
⎢ ⎥        ⎢                                                                  ⎥⎢       ⎥
⎢Q4 ⎥ = AE ⎢ 0       − 0.333             0    0.333     0       0      0    0⎥ ⎢− 0.025⎥
⎢Q5 ⎥      ⎢ − 0.128 − 0.096             0      0     0.128   0.096    0    0⎥ ⎢ 0 ⎥
⎢ ⎥        ⎢                                                                  ⎥⎢       ⎥
⎢Q6 ⎥      ⎢− 0.096 − 0.072              0      0     0.096   0.072    0    0⎥ ⎢ 0 ⎥
⎢Q ⎥       ⎢ − 0.25     0                0      0       0       0     0.25 0⎥ ⎢ 0 ⎥
⎢ 7⎥       ⎢                                                                  ⎥⎢       ⎥
⎢Q8 ⎥
⎣ ⎦        ⎢ 0
           ⎣            0                0      0       0       0      0    0⎥ ⎢ 0 ⎥
                                                                              ⎦⎣       ⎦
edayedaHRsaysRmab;bMlas;TI ¬smIkar 14-19¦ eyIg)an
                                                                       ⎡ 0 ⎤
                                                                       ⎢− 0.025⎥
                                                                       ⎢       ⎥
⎡0 ⎤     ⎡0.378 0.096⎤ ⎡ D1 ⎤     ⎡0    0    − 0.128 − 0.096 − 0.25 0⎤ ⎢ 0 ⎥
⎢0⎥ = AE ⎢0.096 0.405⎥ ⎢ D ⎥ + AE ⎢0 − 0.333 − 0.096 − 0.072           ⎢
                                                                    0⎥ ⎢ 0 ⎥
                                                                               ⎥
⎣ ⎦      ⎣           ⎦⎣ 2 ⎦       ⎣                            0     ⎦
                                                                       ⎢ 0 ⎥
                                                                       ⎢       ⎥
                                                                       ⎢ 0 ⎥
                                                                       ⎣       ⎦
EdleyIgTTYl)an
           0 = AE [(0.378 D1 + 0.096 D2 ) + 0]

           0 = AE [(0.096 D1 + 0.405 D2 ) + 0.00833]
edayedaHRsayRbB½n§smIkarenH eyIg)an
           D1 = 0.00556m

           D2 = −0.021875m
eTaHbICaeKminRtUvkarKNnakmøaMgRbtikmμTMrk¾eday EtRbsinebIcaM)ac;eKRtUvKNnavaBIkarBnøatEdl
kMNt;edaysmIkar 14-20. edayeRbIsmIkar 14-23 edIm,IkMNt;kmøaMgenAkñúgGgát;elx @ eyIg)an
Ggát;elx @³ λ x = −0.8, λ y = −0.6, L = 5m, AE = 8(103 )kN dUcenH
                                              ⎡ 0.00556 ⎤

           q2 =
                    ( )
                8 10 3
                       [0.8 0.6 − 0.8 − 0.6]⎢
                                              ⎢− 0.02187 ⎥
                                                         ⎥
                   5                          ⎢     0    ⎥
                                              ⎢          ⎥
                                              ⎣     0    ⎦

              =
                8 10( )
                     3
                       (0.00444 − 0.0131) = −13.9kN
                   5
edayeRbIdMeNIrkarKNnadUcKña bgðajfakmøaMgenAkñúgGgát;elx ! KW q1 = 8.34kN ehIykmøaMgenAkñúg
Ggát;elx # KW q3 = 11.1kN . lT§plRtUv)anbgðajenAkñúgdüaRkamGgÁesrIrbs;tMN ② ¬rUbTI 14-
11c¦ EdleKGacepÞógpÞat;edaysmIkarlMnwg.

 karviPaK truss edayeRbIviFIPaBrwgRkaj                                               T.Chhay   -486
mhaviTüal½ysMNg;sIuvil                                                 viTüasßanCatiBhubec©keTskm<úCa

!$>&> kUGredaenrbs; node (Nodal coordinates)
        enAeBlTMrkl;rbs; truss sßitenAelIbøg;eRTt ehIyeKGackMNt;PaBdabsUnüenARtg;TMreday
eRbIRbB½n§kUGredaenskltamTisedk nigtamTisQrEtmYy. ]TahrN_ eKman truss enAkñúgrUbTI 14-
12a. eKRtUvkMNt;lkçxNÐénbMlas;TIsUnüenARtg;tMN ① tambeNþayG½kS y' ' ehIyedaysarTMr
kl;Gacpøas;TItambeNþayG½kS x' ' dUcenH node enHRtUvmanbgÁúMbMlas;TItamG½kSkUGredaen x, y .
sRmab;mUlehtuenH eyIgminGacrYmbBa©ÚllkçxNÐbMlas;TIsUnüenARtg; node enH enAeBlsresr
smIkarPaBrwgRkajsklsRmab; truss edayeRbIG½kS x, y edaymineFVIeGaymankarEktRmUvdMeNIr
karviPaKm:aRTIs.




        edIm,IedaHRsaycMeNaTenH eyIgGacbBa©ÚlvaeTAkñgkarviPaKkMuBüÚT½redayRsYl eyIgnwgeRbIsMnMu
                                                          ú
kUGredaenrbs; node x' ' , y' ' enARtg;TMreRTt. eKRtUveFVIeGayG½kSTaMgenHmanTItaMgy:agNaedIm,I
eGaykmøaMgRbtikmμTMr nigbMlas;TIrbs;TMrpøas;TItambeNþayG½kSkUGredaennImYy² ¬rUbTI 14-12a¦.
edIm,IKNnasmIkarPaBrwgRkajsklsRmab; truss enaHeKcaM)ac;begáItm:aRTIsbMElgkmøaMg nigma:RTIs
bMElgbMlas;TIsRmab;Ggát;EdltP¢ab;eTAnwgTMrenaH dUcenHeKGaceFVIplbUklT§plTaMgenHenAkñúgRbB½n§
kUGredaenskl x, y dUcKña. edIm,IbgðajBIrebobénkarGnuvtþ eyIgRtUvBicarNaGgát; truss elx! enA
Truss analysis using the stiffness method                                       T.Chhay   -487
Department of Civil Engineering                                                               NPIC



kñúgrUbTI 14-12b EdlmanRbB½n§kUGredaenskl x, y enARtg;cugCit N ehIyRbB½n§kUGredaenrbs;
node x' ' , y ' ' enARtg;cugq¶ay F . enAeBlbMlas;TI D ekIteLIg dUcenHBYkvamanbgÁúMtambeNþayG½kS

nImYy²dUcbgðajenAkñúgrUbTI 14-12c enaHbMlas;TItamTis x tambeNþaycugGgát;nImYy²køayCa
           d N = D N x cos θ x + D N y cos θ y

           d F = DFx '' cos θ x '' + DFy '' cos θ y ''

eKGacsresrsmIkarTaMgenHenAkñúgTRmg;m:aRTIs
                                                    ⎡ DN x ⎤
                                                    ⎢         ⎥
           ⎡ d N ⎤ ⎡λ x λ y 0               0 ⎤ ⎢ DN y ⎥
           ⎢d ⎥ = ⎢ 0 0 λ                  λ y '' ⎥ ⎢ DFx '' ⎥
           ⎣ F⎦ ⎣           x ''                  ⎦⎢          ⎥
                                                    ⎢ D Fy '' ⎥
                                                    ⎣         ⎦
dUcKña kmøaMg q enARtg;cugCit nigcugq¶ayrbs;Ggát; ¬rUbTI 14-12d¦ manbgÁúM Q tambeNþayG½kSskl
           Q N x = q N cos θ x                      Q N y = q N cos θ y

          Q Fx '' = q F cos θ x ''                  Q Fy '' = q F cos θ y ''

EdleKGacsresrCa
           ⎡ Q N x ⎤ ⎡λ x 0 ⎤
           ⎢Q ⎥ ⎢                ⎥
           ⎢ N y ⎥ = ⎢λ y 0 ⎥ ⎡ q N ⎤
           ⎢Q Fx '' ⎥ ⎢ 0 λ x '' ⎥ ⎢ q F ⎥
                                   ⎣ ⎦
           ⎢        ⎥ ⎢          ⎥
           ⎢Q Fy '' ⎥ ⎢ 0 λ y '' ⎥
           ⎣        ⎦ ⎣          ⎦
eKeRbIm:aRTIsbMElgbMlas;TI nigm:aRTIskmøaMgenAkñúgsmIkarxagelIedIm,IbegáItm:aRTIsPaBrwgRkaj
sRmab;Ggát;enAkñúgsßanPaBenH. edayGnuvtþsmIkar 14-15 eyIg)an
           k = T T k 'T
               ⎡λ x 0 ⎤
               ⎢λ         ⎥
           k=  ⎢ y 0 ⎥ AE ⎡ 1 − 1⎤ ⎡λ x λ y 0        0 ⎤
                              ⎢− 1 1 ⎥ ⎢ 0 0 λ
               ⎢ 0 λ x '' ⎥ L ⎣                            ⎥
                                     ⎦⎣        x '' λ y '' ⎦
               ⎢          ⎥
               ⎢ 0 λ y '' ⎥
               ⎣          ⎦
edayKNnam:aRTIsxagelI eyIgTTYl)an
                 ⎡ λ2   x        λ x λ y − λ x λ x '' − λ x λ y '' ⎤
                 ⎢                                                      ⎥
              AE ⎢ λ x λ y        λ2 y       − λ y λ x '' − λ y λ y '' ⎥
           k=                                                                       (14-24)
               L ⎢ − λ x λ x '' − λ y λ x ''   λ2 ''      λ x '' λ y '' ⎥
                 ⎢                                 x                    ⎥
                 ⎢− λ x λ y '' − λ y λ y '' λ x '' λ y ''   λ2 '' ⎥
                 ⎣                                               y      ⎦
bnÞab;mkeKGaceRbIm:aRTIsPaBrwgRkajsRmab;Ggát;nImYy²EdlRtUvtP¢ab;eTAnwgTMrkl;EdleRTt ehIy
dMeNIrkarpÁúMm:aRTIsedIm,IbegáItm:aRTIsPaBrwgRkajrcnasm<½n§GnuvtþtamdMeNIrkarbTdæan. ]TahrN_xag
 karviPaK truss edayeRbIviFIPaBrwgRkaj                                             T.Chhay   -488
mhaviTüal½ysMNg;sIuvil                                              viTüasßanCatiBhubec©keTskm<úCa

eRkambgðajBIkarGnuvtþrbs;va.

]TahrN_ 14-6³ kMNt;kmøaMgRbtikmμTMrsRmab; truss dUcbgðajenAkñúgrUbTI 14-13a.




dMeNaHRsay³
kareFVIkMNt;smÁal;³edaysarTMrkl;enARtg; ② sßitenAelIbøg;eRTt eyIgRtUveRbIkUGredaenrbs; node
enARtg; node enH. eKRtUvkMNt;elxerogeGaytMN nigGgát; ehIybegáItkUGredaen x, y enARtg; node
③ ¬rUbTI 14-13b¦. cMNaMfa elxkUd # nig$ sßitenAtambeNþayG½kS x' ' , y ' ' edIm,IeRbIlkçxNÐ

Edl D4 = 0 .
m:aRTIsPaBrwgRkajsRmab;Ggát;³ eKRtUvbegáItm:aRTIsPaBrwgRkajsRmab;Ggát;elx ! nigelx @ eday
eRbIsmIkar 14-24 edaysarGgát;TaMgenHmanelxkUdtamTisénG½kSskl nigG½kSrbs;kUd. eKRtUv
kMNt;m:aRTIsPaBrwgRkajsRmab;Ggát;elx # tamrebobFmμta.
Ggát;elx !³ rUbTI 14-13c/ λ x = 1, λ y = 0, λ x'' = 0.707, λ y'' = −0.707

Truss analysis using the stiffness method                                    T.Chhay   -489
Department of Civil Engineering                                                                        NPIC


                         5               6     3       4
                   ⎡ 0.25                0 − 0.17675 0.17675⎤ 5
                   ⎢                                     0 ⎥6
           k1 = AE ⎢    0                0     0             ⎥
                   ⎢− 0.17675            0   0.125   − 0.125 ⎥ 3
                   ⎢                                         ⎥
                   ⎣ 0.17675             0 − 0.125    0.125 ⎦ 4

Ggát;elx @³ rUbTI 14-13d/ λ x = 0,             λ y = −1, λ x '' = −0.707, λ y '' = −0.707
                     1     2       3     4
                    ⎡ 0    0       0      0   ⎤1
                    ⎢0 0.333 − 0.2357 − 0.2357⎥
           k 2 = AE ⎢                         ⎥2
                    ⎢0 − 0.2357 0.1667 0.1667 ⎥ 3
                    ⎢                         ⎥
                    ⎣0 − 0.2357 0.1667 0.1667 ⎦ 4

Ggát;elx #³ λ x = 0.8,            λ y = 0.6
                      1      2       3        4
                    ⎡ 0.128    0.096 − 0.128 − 0.096⎤ 5
                    ⎢ 0.096    0.072 − 0.0.96 − 0.072⎥ 6
           k 3 = AE ⎢                                ⎥
                    ⎢− 0.128 − 0.096 0.128     0.096 ⎥ 1
                    ⎢                                ⎥
                    ⎣− 0.096 − 0.072 0.0.96    0.072 ⎦ 2

m:aRTIsPaBrwgRkajsRmab;rcnasm<½n§³ pÁúMm:aRTIsTaMgenHedIm,IkMNt;m:aRTIsPaBrwgRkajsRmab;rcna
sm<½n§ eyIg)an
⎡ 30 ⎤   ⎡ 0.128    0.096      0        0    − 0.128 − 0.096⎤ ⎡ D1 ⎤
⎢0⎥      ⎢ 0.096    0.4053 − 0.2357 − 0.2357 − 0.096 − 0.072⎥ ⎢ D2 ⎥
⎢ ⎥      ⎢                                                  ⎥⎢ ⎥
⎢0⎥      ⎢ 0       − 0.2357 0.2917   0.0417 − 0.17675   0 ⎥ ⎢ D3 ⎥
⎢ ⎥ = AE ⎢                                                  ⎥⎢ ⎥
⎢Q4 ⎥    ⎢ 0       − 0.2357  0.417   0.2917  0.17375    0 ⎥⎢ 0 ⎥
⎢Q5 ⎥    ⎢ − 0.128 − 0.096 − 0.17675 0.17675  0.378   0.096 ⎥ ⎢ 0 ⎥
⎢ ⎥      ⎢                                                  ⎥⎢ ⎥
⎢Q6 ⎥
⎣ ⎦      ⎢− 0.096 − 0.072
         ⎣                     0        0     0.096   0.072 ⎥ ⎢ 0 ⎥
                                                            ⎦⎣ ⎦
edayeFVIplKuNm:aRTIsénm:aRTIsEpñkxagelI enaHeyIgGackMNt;bMlas;TI D EdlCaGBaØatBIkaredaH
RsayRbB½n§smIkar eBalKW
                352.5
           D1 =
                 AE
                − 157.5
           D2 =
                  AE
                − 127.3
           D3 =
                  AE
eKGacTTYl)ankmøaMgRbtikmμ Q BIplKuNm:aRTIsénm:aRTIsxageRkamenAkñúgsmIkar (1). edayeRbI
bMlas;TIEdl)anKNna eyIg)an
           Q4 = 0(352.5) − 0.2357(− 157.5) + 0.0417(− 127.3)


 karviPaK truss edayeRbIviFIPaBrwgRkaj                                                      T.Chhay   -490
mhaviTüal½ysMNg;sIuvil                                                    viTüasßanCatiBhubec©keTskm<úCa

                = 31.8kN
           Q5 = −0.128(352.5) − 0.096(− 157.5) − 0.17675(− 127.3)

                = −7.5kN
           Q6 = −0.096(352.5) − 0.072(− 157.5) + 0(− 127.3)

                = −22.5kN


!$>*> Trusses EdlmanbMErbMrYlsItuNðaPaB nigkMhusénplitkmμ
(Truss having thermal changes and fabrication errors)
         RbsinebIGgát;xøHrbs; truss rgnUvkarlUt b¤rYjEdlbNþalBIbMErbMrYlsItuNðPaB b¤kMhusén
plitkmμ enaHeKcaM)ac;RtUveRbIviFItRmYtpledIm,ITTYl)andMeNaHRsay. vaRtUvkarbICMhan. dMbUg eK
caM)ac;RtUvKNnakmøaMgbgáb;cugEdlkarBarkarcl½trbs; node EdlbNþalBIsItuNðPaB b¤kMhusén
plitkmμ. CMhanTIBIrKWeKRtUvdak;kmøaMgEdlesμIKña b:uEnþmanTispÞúyKñaenAelI truss Rtg; node ehIyeK
RtUvKNnabMlas;TIrbs; node edayeRbIkarviPaKm:aRTIs. cugeRkay eKkMNt;kmøaMgCak;EsþgenAkñúg
Ggát; nigkmøaMgRbtikmμenAelI truss edaykareFVItRmYtplénlT§plTaMgBIrenH. Cak;Esþg eKRtUvkar
dMeNIrkarenH RbsinebI truss Carcnasm<½n§minkMNt;edaysþaTic. RbsinebI truss Carcnasm<½n§kMNt;
edaysþaTic eKGackMNt;bMlas;TIenARtg; node edayviFIenH b:uEnþbMErbMrYlsItuNðPaB nigkMhusén
plitkmμnwgminmanT§iBleTAelIkmøaMgRbtikmμ nigkmøaMgkñúgrbs;Ggát; edaysareKGacEktRmUvbERm
bRmYlRbEvgrbs;Ggát; truss edayesrI.
T§iBlkMedA³ RbsinebIGgát; truss manRbEvg
 L rgkMeNInsItuNðPaB ΔT RbEvgrbs;Ggát;

nwgmankMhUcRTg;RTay ΔL = αΔTL Edl α Ca
emKuNrIkedaysarkMedA. kmøaMgsgát; qo Edl
GnuvtþeTAelIGgát;nwgeFVIeGayRbEvgrbs;Ggát;
rYj)anRbEvg ΔL' = qo L / AE . RbsinebIeyIg
dak;eGaybMlas;TITaMgBIresμIKña enaH qo =
 AEαΔT . kmøaMgenHnwgTb;Ggát;dUcbgðajenAkñúgrUbTI 14-14 dUcenHeyIg)an

                      (q N )0 = AEαΔT
                      (q F )0 = − AEαΔT

Truss analysis using the stiffness method                                          T.Chhay   -491
Department of Civil Engineering                                                             NPIC



eKRtUvdwgfa RbsinekItmankarfykMedA enaH ΔT køayCaGviC¢man ehIykmøaMgTaMgenHnwgbRBa©asTisedA
edIm,IeFVIeGayGgát;sßitenAkñúgsßanPaBlMnwg.
           eyIgGacbMElgkmøaMgTaMgBIrenHeTAkñúgkUGredaenskledayeRbIsmIkar 14-10 EdleFVIeGay
            (
           ⎡ QN x   )0 ⎤ ⎡λ x 0 ⎤                    ⎡ λx ⎤
            ( )
           ⎢Q
           ⎢ Ny
                     ⎥ ⎢
                           λ
                    0⎥ = ⎢ y
                              0⎥ ⎥
                                       ⎡1⎤
                                                     ⎢λ ⎥
                                                     ⎢ y ⎥
            ( )
           ⎢ QF      ⎥ ⎢ 0 λ x ⎥ AEαΔT ⎢− 1⎥ = AEαΔT ⎢ − λ x ⎥
                                       ⎣ ⎦
                                                                                  (14-25)

            ( )
           ⎢ x
           ⎢ Q Fy
           ⎣
                    0⎥

                    0⎥ ⎢
                     ⎦ ⎣
                         ⎢       ⎥
                            0 λy ⎥
                                 ⎦
                                                     ⎢
                                                     ⎢− λ y ⎥
                                                     ⎣
                                                             ⎥
                                                             ⎦
kMhusqÁgkñúgplitkmμ³ RbsinebIeKeFVIeGayGgát;EvgCaRbEvgedImedayTMhM ΔL muxeBlP¢ab;vaeTAnwg
truss enaHkmøaMg qo EdlcaM)ac;edIm,IrkSaGgát;RtwmRbEvgDIsaj L KW qo = AEΔL / L dUcenHsRmab;

Ggát;enAkñúgrUbTI 14-14 eyIg)an
                                AEΔL
                     (q N )0 =
                                  L
                                  AEΔL
                     (q F )0   =−
                                    L
RbsinebIGgát;enHxøICagRbEvgedIm enaH ΔL køayCaGviC¢man ehIykmøaMgTaMgenHnwgbRBa©as.
       enAkñúgkUGredaenskl kmøaMgTaMgenHKW
                       (
                     ⎡ QN x    )0 ⎤          ⎡ λx ⎤
                     ⎢Q( )
                     ⎢ Ny
                                    ⎥        ⎢λ ⎥
                                  0 ⎥ = AEΔL ⎢ y ⎥
                       ( )
                     ⎢ QF           ⎥    L ⎢− λ x ⎥
                                                                                  (14-26)

                       ( )
                     ⎢ x
                     ⎢ Q Fy
                     ⎣
                                  0⎥

                                  0⎦⎥
                                             ⎢
                                             ⎣
                                                    ⎥
                                             ⎢− λ y ⎥
                                                    ⎦
karviPaKm:aRTIs³ enAkñúgkrNITUeTA CamYy truss rgkmøaMgGnuvtþ bERmbRmYlsItuNðPaB nigkMhusén
plitkmμ TMnak;TMngrvagkmøaMgkñúg nigbMlas;TIsRmab; truss enaHvakøayCa
                     Q = KD + Q0                                                  (14-27)
enATIenH Q0 Cam:aRTIsCYrQrsRmab; truss TaMgmUlrbs;kmøaMgbgáb;cugEdlbNþalBIbERmbRmYl
sItuNðPaB nigkMhusénplitkmμrbs;Ggát;EdlkMNt;enAkñúgsmIkar 14-25 nig 14-26. eyIgGacEbg
EcksmIkarenHenAkñúgTRmg;dUcxageRkam
                     ⎡Qk ⎤ ⎡ K11 K12 ⎤ ⎡ Du ⎤ ⎡(Qk )0 ⎤
                     ⎢Q ⎥ = ⎢ K      ⎥⎢ ⎥ + ⎢         ⎥
                     ⎣ u ⎦ ⎣ 21 K 22 ⎦ ⎣ Dk ⎦ ⎣(Qu )0 ⎦
edayedaHRsaym:aRTIsenAGgÁxagsþaM eyIgTTYl)an
                     Qk = K11 Du + K 21 Dk + (Qk )0                               (14-28)
                     Qu = K 21 Du + K 22 Dk + (Qu )0                              (14-29)




 karviPaK truss edayeRbIviFIPaBrwgRkaj                                           T.Chhay   -492
mhaviTüal½ysMNg;sIuvil                                                         viTüasßanCatiBhubec©keTskm<úCa

eyagtamdMeNIrkartRmYtplEdlerobrab;xagelI eyIgGackMNt;bMlas;TI Du BIsmIkarTImYyedaydk
 K12 Dk nig (Qk )0 BIGgÁTaMgBIr bnÞab;mkeyIgedaHRsay Du . eyIgTTYl)an

                      Du = K111 (Qk − K12 Dk − (Qk )0 )
                            −


eRkayeBleyIgTTYl)anbMlas;TIrbs; node enaHeyIgGackMNt;kmøaMgkñúgrbs;Ggát;edayviFItRmYtpl
eBalKW
                      q = k ' TD + q0
RbsinebIeyIgBnøatsmIkarenHedIm,IkMNt;kmøaMgenAcugq¶ayrbs;Ggát; eyIgTTYl)an
                                                       ⎡ DN x ⎤
                                                       ⎢D ⎥
                      qF =
                               AE
                                L
                                    [
                                  − λx − λ y λx       ]
                                                   λ y ⎢ y ⎥ − (q F )0
                                                          N
                                                       ⎢ DFx ⎥
                                                                                             (14-30)
                                                       ⎢      ⎥
                                                       ⎢ D Fy ⎥
                                                       ⎣      ⎦
lT§plenHRsedogKñaeTAnwgsmIkar 14-23 EtvaxusKñaRtg;enATIenHvamanplbUkéntY (q F )0 EdlCa
kmøaMgbgáb;cugrbs;Ggát;EdlbNþalBIbERmbRmYlsItuNðPaB nig / b¤kMhusénplitkmμdUckMNt;dUcxag
elI. eKRtUvdwgfa RbsinebIlT§plEdlTTYl)anBIsmIkarenHmantémøGviC¢man enaHGgát;nwgrgkmøaMg
sgát;.
       ]TahrN_TaMgBIrxageRkam nwgbgðajBIkarGnuvtþéndMeNIrkarrbs;viFIenH.

]TahrN_ 14-7³ kMNt;kmøaMgkñúgGgát;elx ! nig
elx @ rbs; truss EdlmanTMrsnøak;dUcbgðajenA
kñúgrUbTI 14-15 RbsinebIeKeFVIeGayGgát;elx @
xøICagmun 0.01 munnwgpÁúMvaeTAkñúg truss. yk AE =
8(10 3 )kN .



dMeNaHRsay³
edaysarGgát;manRbEvgxøI enaH ΔL = −0.01m
dUcenHGnuvtþsmIkar 14-26 eTAelIGgát;elx @ CamYy nwg λ x = −0.8,           λ y = −0.6   eyIg)an
                      ⎡ (Q1 )0 ⎤            ⎡ − 0.8 ⎤      ⎡ 0.0016 ⎤ 1
                      ⎢(Q ) ⎥               ⎢ − 0.6 ⎥      ⎢        ⎥
                      ⎢ 2 0 ⎥ = AE (− 0.01) ⎢       ⎥ = AE ⎢ 0.0012 ⎥ 2
                      ⎢(Q5 )0 ⎥     5       ⎢ 0.8 ⎥        ⎢− 0.0016⎥ 5
                      ⎢        ⎥            ⎢       ⎥      ⎢        ⎥
                      ⎢(Q6 )0 ⎥
                      ⎣        ⎦            ⎣ 0.6 ⎦        ⎣− 0.0012⎦ 6
Truss analysis using the stiffness method                                               T.Chhay   -493
Department of Civil Engineering                                                                   NPIC



eK)anbegáItm:aRTIsPaBrwgRkajsRmab;rcnasm<n§enAkñúg]TahrN_ 14-4. edayGnuvtþsmIkar 14-27
                                         ½
eyIg)an
⎡0⎤        ⎡ 0.378 0.096                 0    0    − 0.128 − 0.096 − 0.25 0⎤ ⎡ D1 ⎤      ⎡ 0.0016 ⎤
⎢0⎥        ⎢ 0.096 0.405                 0 − 0.333 − 0.096 − 0.072   0     ⎥⎢D ⎥
                                                                          0⎥ ⎢ 2 ⎥       ⎢ 0.0012 ⎥
⎢ ⎥        ⎢                                                                             ⎢        ⎥
⎢Q3 ⎥      ⎢ 0          0                0    0       0       0      0    0⎥ ⎢ 0 ⎥       ⎢    0   ⎥
⎢ ⎥        ⎢                                                               ⎥⎢ ⎥          ⎢        ⎥
⎢Q4 ⎥ = AE ⎢ 0       − 0.333             0 0.333      0       0      0    0⎥ ⎢ 0 ⎥       ⎢    0   ⎥
                                                                                    + AE
⎢Q5 ⎥      ⎢ − 0.128 − 0.096             0    0     0.128 0.096      0    0⎥ ⎢ 0 ⎥       ⎢− 0.0016⎥
⎢ ⎥        ⎢                                                               ⎥⎢ ⎥          ⎢        ⎥
⎢Q6 ⎥      ⎢− 0.096 − 0.072              0    0     0.096 0.072      0    0⎥ ⎢ 0 ⎥       ⎢− 0.0012⎥
⎢Q ⎥       ⎢ − 0.25     0                0    0       0       0     0.25 0⎥ ⎢ 0 ⎥        ⎢    0   ⎥
⎢ 7⎥       ⎢                                                               ⎥⎢ ⎥          ⎢        ⎥
⎢Q8 ⎥
⎣ ⎦        ⎢ 0
           ⎣            0                0    0       0       0      0    0⎥ ⎢ 0 ⎥
                                                                           ⎦⎣ ⎦          ⎢
                                                                                         ⎣    0   ⎥
                                                                                                  ⎦
edayEbgEckm:aRTIsenHdUcbgðaj nigedayedaHRsayplKuNm:aRTIsedIm,ITTYl)ansmIkarsRmab;
bMlas;TI eyIgTTYl)an
                                                                       ⎡0⎤
                                                                       ⎢0⎥
                                                                       ⎢ ⎥
⎡0 ⎤     ⎡0.378 0.096⎤ ⎡ D1 ⎤     ⎡0    0    − 0.128 − 0.096 − 0.25 0⎤ ⎢0⎥      ⎡0.0016⎤
⎢0⎥ = AE ⎢0.096 0.405⎥ ⎢ D ⎥ + AE ⎢0 − 0.333 − 0.096 − 0.072         ⎥ ⎢0⎥ + AE ⎢0.0012⎥
⎣ ⎦      ⎣           ⎦⎣ 2 ⎦       ⎣                            0    0⎦ ⎢ ⎥      ⎣      ⎦
                                                                       ⎢0⎥
                                                                       ⎢ ⎥
                                                                       ⎢0⎥
                                                                       ⎣ ⎦
EdleGay
           0 = AE [0.378 D1 + 0.096 D2 ] + AE [0] + AE [0.0016]

           0 = AE [0.096 D1 + 0.405 D2 ] + AE [0] + AE [0.0012]
edaHRsayRbB½n§smIkar eyIgTTYl)an
                     D1 = −0.003704m

                     D2 = −0.002084m
eTaHbICaminRtUvkar eKGackMNt;kmøaMgRbtikmμ Q BIkarBnøatsmIkar (1) EdlGnuvtþtamKMrUénsmIkar
14-29.

        edIm,IkMNt;kmøaMgenAkñúgGgát;elx ! nigelx @ eyIgRtUvGnuvtþsmIkar 14-30 EdlenAkñúgkrNI
enH eyIg)an
Ggát;elx !³ λ x = 0, λ y = 1, L = 3m, AE = 8(103 )kN dUcenH
                                  ⎡     0    ⎤

           q1 =
                   ( )
                8 10 3
                       [0 − 1 0 1]
                                  ⎢
                                  ⎢     0    ⎥
                                             ⎥ + [0]
                   3              ⎢− 0.003704⎥
                                  ⎢          ⎥
                                  ⎣− 0.002084⎦

 karviPaK truss edayeRbIviFIPaBrwgRkaj                                                 T.Chhay   -494
mhaviTüal½ysMNg;sIuvil                                                                  viTüasßanCatiBhubec©keTskm<úCa

           q1 = −5.56kN
Ggát;elx @³ λ x = −0.8,                                             ( ) dUcenH
                                    λ y = −0.6, L = 5m, AE = 8 10 3 kN
                                            ⎡− 0.003704⎤

           q2 =
                     ( )
                8 10 3
                                            ⎢− 0.002084⎥
                       [0.8 0.6 − 0.8 − 0.6]⎢          ⎥ − 8 10 (− 0.01)
                                                               3
                                                                          ( )
                   5                        ⎢     0    ⎥         5
                                            ⎢          ⎥
                                            ⎣     0    ⎦
           q 2 = 9.26kN



]TahrN_ 14-8³ Ggát;elx @ rbs;                Edl     truss

bgðajenA kñúgrUbTI 14-16 rgnUvkMeNInsItuNðPaB
83.3o C . kMNt;kmøaMgEdlekItmanenAkñúgGgát;elx @.

yk α = 11.7(10 −6 )/ o C / E = 200GPa . Ggát;
nImYy²manRkLaépÞmuxkat; A = 484mm 2 .

dMeNaHRsay³
edaysar vamankMeNInsItuNðPaB ΔT = +83.3o C . GnuvtþsmIkar 14-25 eTAelIGgát;elx @ Edl
λ x = 0.707, λ y = 0.707 eyIg)an
           ⎡ (Q1 )0 ⎤                       ⎡ 0.707 ⎤       ⎡ 0.000689325 ⎤ 1
           ⎢(Q ) ⎥                          ⎢ 0.707 ⎥       ⎢             ⎥
           ⎢ (Q3 )0 ⎥
                                        ( )
           ⎢ 2 0 ⎥ = AE (11.7 ) 10 −6 (83.3)⎢        ⎥ = AE ⎢ 0.000689325 ⎥ 2
                                            ⎢− 0.707 ⎥      ⎢− 0.000689325⎥ 7
           ⎢        ⎥                       ⎢        ⎥      ⎢             ⎥
           ⎣(Q4 )0 ⎦                        ⎣− 0.707 ⎦      ⎣− 0.000689325⎦ 8
m:aRTIsPaBrwgRkajsRmab; truss enHRtUv)anbegáItenAkñúg]TahrN_ 14-2.
⎡ 0 ⎤      ⎡ 0.135         0.035       0      0       0    − 0.1 − 0.035 − 0.035⎤ ⎡ D1 ⎤       ⎡ 0.000689325 ⎤ 1
⎢ 0 ⎥      ⎢ 0.035                                                               ⎥ ⎢D ⎥        ⎢ 0.000689325 ⎥ 2
⎢ ⎥        ⎢              0.135    0         − 0.1    0      0    − 0.035 − 0.035⎥ ⎢ 2 ⎥       ⎢             ⎥
⎢ 0 ⎥      ⎢ 0              0    0.135      − 0.035 0.035 − 0.035 − 0.1      0 ⎥ ⎢ D3 ⎥        ⎢       0     ⎥3
⎢ ⎥        ⎢                                                                     ⎥⎢ ⎥          ⎢             ⎥
⎢ 0 ⎥ = AE ⎢ 0            − 0.1 − 0.035      0.135 − 0.035 0.035             0 ⎥ ⎢ D4 ⎥
                                                                                          + AE ⎢             ⎥4
                                                                     0                                 0
⎢ 0 ⎥      ⎢ 0              0    0.035      − 0.035 0.135 − 0.035    0     − 0.1 ⎥ ⎢ D5 ⎥      ⎢       0     ⎥5
⎢ ⎥        ⎢                                                                     ⎥⎢ ⎥          ⎢             ⎥
⎢Q 6 ⎥     ⎢ − 0.1          0   − 0.035      0.035 − 0.035 0.135     0       0 ⎥⎢ 0 ⎥          ⎢       0     ⎥6
⎢Q ⎥       ⎢− 0.035      − 0.035 − 0.1         0      0      0     0.135 0.035   ⎥⎢ 0 ⎥        ⎢− 0.000689325⎥ 7
⎢ 7⎥       ⎢                                                                     ⎥⎢ ⎥          ⎢             ⎥
⎣Q8 ⎥
⎢ ⎦        ⎢− 0.035
           ⎣             − 0.035       0       0    − 0.1    0     0.035 0.135 ⎥ ⎢ 0 ⎥
                                                                                 ⎦⎣ ⎦          ⎢− 0.000689325⎥ 8
                                                                                               ⎣             ⎦

edayBnøatedIm,IkMNt;smIkarbMlas;TIEdlCaGBaØat nigedayedaHRsayRbB½n§smIkarenH eyIg)an
           D1 = −0.002027m

           D2 = −0.01187 m

Truss analysis using the stiffness method                                                        T.Chhay   -495
Department of Civil Engineering                                                                               NPIC



           D3 = −0.002027m

           D4 = −0.009848m
           D5 = −0.002027m
edayeRbIsmIkar 14-30 edIm,IkMNt;kmøaMgenAkñúgGgát;elx @ eyIg)an
                                                      ⎡− 0.002027⎤
                                                      ⎢ − 0.01187 ⎥
                484[200]
           q2 =
                 10 2
                         [− 0.707 − 0.707 0.707 0.707]⎢
                                                      ⎢      0
                                                                  ⎥ − 484(200)11.7 10 −6 (83.3)
                                                                  ⎥
                                                                                                  [ ( )]
                                                      ⎢           ⎥
                                                      ⎣      0    ⎦

               = −27.09kN
cMNaMfa kMeNInsItuNðPaBénGgát;elx @ nwgmineFVIeGaymankmøaMgRbtikmμenAelI truss eT edaysarva
Ca truss kMNt;edaysþaTic. edIm,IbgðajBIkarBicarNakarBnøatm:aRTIsénsmIkar (1) edIm,IkMNt;kmøaMg
Rbtikmμ. edayeRbIlT§plsRmab;bMlas;TI eyIg)an
Q6 = AE[− 0.1(− 0.002027 ) + 0 − 0.035(− 0.002027 ) + 0.035(− 0.009828) − 0.035(− 0.002027 )]

           + AE [0] = 0
Q7 = AE[− 0.035(− 0.002027 ) − 0.035(− 0.01187 ) − 0.1(− 0.002027 ) + 0 + 0]

           + AE [− 0.000689325] = 0
Q8 = AE[− 0.035(− 0.002027 ) − 0.035(− 0.01187 ) + 0 + 0 − 0.1(− 0.002027 )]

           + AE [− 0.000689325] = 0



!$>(> karviPaK truss kñúglMh (Space-truss analysis)
        eKGacviPaK truss kñúglMhkMNt;edaysþaTic nig truss kñúglMhminkMNt;edaysþaTicedayeRbI
dMeNIrkarviPaKdUcKñaEdl)anerobrab;BIelIkmun. b:uEnþ edIm,IKitG½kSTaMgbI eKRtUvbBa©ÚlFatubEnßmeTAkñúg
m:aRTIsbMElg T . edIm,ITTYl)anva eyIgnwgBicarNaGgát; truss EdlbgðajenAkñúgrUbTI 14-17.
m:aRTIsPaBrwgRkajsRmab;Ggát;EdlkMNt;edayeRbIkUGredaentMbn; x' RtUv)aneGayedaysmIkar 14-4.
elIsBIenH tamkarGegátrUbTI 14-17 eKGackMNt;kUsIunUsR)ab;TiscenøaHkUGredaenskl nigkUGr-
edaentMbn;edayeRbIsmIkarRsedogKñanwgsmIkar 14-5 nig 14-6 Edl
                                  xF − xN                        xF − xN
           λ x = cos θ x =                =                                                         (14-31)
                                     L        (x F   − x N )2 + ( y F − y N )2 + ( z F − z N )2
                                  yF − yN                         yF − yN
           λ y = cos θ y =                =                                                         (14-32)
                                     L        (x F   − x N ) + ( y F − y N ) + (z F − z N )
                                                            2                2                2



 karviPaK truss edayeRbIviFIPaBrwgRkaj                                                             T.Chhay   -496
mhaviTüal½ysMNg;sIuvil                                                                        viTüasßanCatiBhubec©keTskm<úCa
                                zF − zN                             zF − zN
           λ z = cos θ z =              =                                                                   (14-33)
                                   L             (x F   − x N )2 + ( y F − y N )2 + ( z F − z N )2

CalT§plénTMhM ¬G½kS¦TIbI m:aRTIsbMElg ¬smIkar 14-9¦ køayCa
              ⎡λ x λ y λ z 0 0 0 ⎤
           T =⎢                  ⎥
              ⎣ 0 0 0 λx λ y λz ⎦
edayCMnYsm:aRTIsenH nigsmIkar 14-4 eTAkñúgsmIkar 14-15 ¬ K = T T k 'T ¦ eyIg)an
             ⎡λ x        0⎤
             ⎢λ          0⎥
             ⎢ y            ⎥
             ⎢λ          0 ⎥ AE ⎡ 1 − 1⎤ ⎡λ x λ y λ z 0 0 0 ⎤
           k=⎢ z            ⎥            ⎢                   ⎥
             ⎢0         λ x ⎥ L ⎢− 1 1 ⎥ ⎣ 0 0 0 λ x λ y λ z ⎦
                                ⎣      ⎦
             ⎢0         λy ⎥
             ⎢              ⎥
             ⎢0
             ⎣          λz ⎥⎦
edayedaHRsayplKuNm:aRTIs eyIgnwgTTYl)anm:aRTIssIuemRTI
                  Nx          Ny            Nz     Fx         Fy        Fz
      ⎡ λ2  x              λxλ y       λxλz      − λ2
                                                    x    − λxλ y − λxλz ⎤ N x
      ⎢                                                                   ⎥
      ⎢ λ y λx               λ2
                              y        λ y λ z − λ y λ x − λ2 − λ y λ z ⎥ N y
                                                                y
   AE ⎢
k=      λz λx              λz λ y       λ z − λ z λ x − λ z λ y − λ2 ⎥ N z
                                           2
                                                                                                            (14-34)
    L ⎢
                                                                       z ⎥
      ⎢ − λ2  x          − λxλ y      − λxλz     λx2
                                                          λ x λ y λ x λ z ⎥ Fx
      ⎢                                                                   ⎥
      ⎢− λ y λ x           − λ2
                              y       − λ y λz λ y λx      λ2 y   λ y λ z ⎥ Fy
      ⎢− λ λ              − λz λ y     − λ2 λ z λ x λ z λ y        λ2 ⎥ Fz
      ⎣ z x                                  z                        z ⎦

smIkarenHCam:aRTIsPaBrwgRkajsRmab;Ggát;Edl
sresredayeRbIkUGredaenskl. elxkUdtam
beNþayCYredk nigCYrQrtMNageGayTis x, y, z
enARtg;cugCit N x , N y , N z Edlbnþedaycugq¶ay
 Fx , F y , Fz .

         sRmab;karsresrkmμviFIkMuBüÚT½r CaTUeTAvaman
lkçN³gayRsYlkñúgkareRbIsmIkar 14-34 Cagkar
edaHRsayplKuNm:aRTIs T T k 'T sRmab;Ggát;
nImYy². dUckarerobrab;BIxagedIm dMbUgkMuBüÚT½rnwg rkSam:aRTIsPaBrwgRkajsRmab;rcnasm½<n§ K Edl
manFatuesμIsUnü bnÞab;mkeTotedaysarFatunImYy² énm:aRTIsPaBrwgRkajsRmab;Ggát;RtUv)anbegáIt
vaRtUv)andak;eTAkñúgTItaMgRtUvKñarbs;vaenAkñúgm:aRTIs K . eRkayeBlFaturbs;m:aRTIsPaBrwgRkaj

Truss analysis using the stiffness method                                                              T.Chhay   -497
Department of Civil Engineering                                                           NPIC



sRmab;rcnasm<½n§RtUv)anbegáIt eKGacGnuvtþdMeNIrkar Edl)anerobrab;enAkñúgkfaxNÐ 14-6 edIm,I
kMNt;bMlas;TIrbs;tMN kmøaMgRbtikmμ nigkmøaMgkñúgrbs; Ggát;.




 karviPaK truss edayeRbIviFIPaBrwgRkaj                                         T.Chhay   -498
mhaviTüal½ysMNg;sIuvil                                            viTüasßanCatiBhubec©keTskm<úCa

                                        cMeNaT
14>1 kMNt;m:aRTIsPaBrwgRkaj K sRmab;eRKOg 14>6 kMNt;m:aRTIsPaBrwgRkaj K sRmab; truss.
bgÁúM. yk A = 300mm 2 nig E = 200GPa      yk A = 0.005m 2 nig E = 200GPa . snμt;
sRmab;Ggát;.                              tMNTaMgGs;tP¢ab;edaysnøak;.




14>2 kMNt;bMlas;TItamTisedk nigTisQr
enARtg;tMN ③ rbs;eRKOgbgÁúMenAkñúgcMeNaT
14>1.
                                              14>7 kMNt;bMlas;TItamTisQrenARtg;tMN ①
14>3 kMNt;kmøaMgkñúgénGgát;nImYy²rbs;eRKOg
                                              nigkmøaMgkñúgrbs;Ggát;elx @ éncMeNaT 14>6.
bgÁúMenAkñúgcMeNaT 14>1.
                                              14>8 kMNt;m:aRTIsPaBrwgRkaj K sRmab; truss.
14>4 kMNt;m:aRTIsPaBrwgRkaj K sRmab; truss.
                                              yk A = 0.0015m 2 nig E = 200GPa sRmab;
yk A = 300mm 2 nig E = 200GPa sRmab;
                                              Ggát;.
Ggát;.




14>5 kMNt;bMlas;TItamTisQrenARtg;tMN ④
nigkmøaMgkñúgrbs;Ggát;elx $ éncMeNaT 14>4.    14>9 kMNt;kmøaMgkñúgénGgát;elx ^ éncMeNaT
yk A = 0.0015m 2 nig E = 200GPa .             14>8. yk A = 0.0015m 2 nig E = 200GPa
Problems                                                                   T.Chhay   -499
Department of Civil Engineering                                                        NPIC



sRmab;Ggát;nImYy².                             14>13. yk A = 1000mm 2 nig E =
14>10 kMNt;kmøaMgkñúgénGgát;elx ! éncMeNaT     200GPa .

14>8 RbsinebI Ggát;EvgCagmun10mm munnwg        14>15 kMNt;kmøaMgkñúgénGgát;elx @éncMeNaT
P¢ab;vaeTAkñúg truss. edIm,IedaHRsay dkbnÞúk   14>8 RbsinebIsItuNðPaBekIneLIg 55o C .
10kN ecj. yk A = 0.0015m 2 nig E =             yk A = 1000mm 2 E = 200GPa nig α =
 200GPa sRmab;Ggát;nImYy².                     11.7(10 −6 )/ o C .

14>11 kMNt;m:aRTIsPaBrwgRkaj K sRmab;          14>16 kMNt;kmøaMgRbtikmμenAelI truss. AE
truss. AE CacMnYnefr.                          CacMnYnefr.




14>12 kMNt;kmøaMgkñúgénGgát;elx @ nig
elx % éncMeNaT 14>11. AE CacMnYnefr.
14>13 kMNt;m:aRTIsPaBrwgRkaj K sRmab;
truss. yk A = 1000mm 2 nig E = 200GPa .




 14>14 kMNt;bMlas;TItamTisedkenARtg;tMN
  ① nigkmøaMgkñúgrbs;Ggát;elx @ éncMeNaT


 cMeNaT                                                                     T.Chhay   -500

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14. truss analysis using the stiffness method

  • 1. Department of Civil Engineering NPIC !$> karviPaK truss edayeRbIviFIPaBrwgRkaj Truss analysis using the stiffness method enAkñúgemeronenH eyIgnwgBnül;BIeKalkarN_mUldæanénkareRbIR)as;viFIPaBrwgRkajsRmab;viPaKeRKOg bgÁúM. viFIenHmanPaBsμúKsμajsRmab;karedaHRsayedayéd EtvasaksmsRmab;eRbICamYynwgkMuBüÚT½r. enAkñúgemeronenHmanbgðajBI]TahrN_Gnuvtþn_eTAelI truss kñúgbøg;. bnÞab;mk eyIgnwgeRbIviFIenH sRmab; truss kñúglMh. eyIgnwgerobrab;BIkarGnuvtþviFIenHsRmab;Fñwm nigeRKagenAemeroneRkay. !$>!> eKalkarN_mUldæanénviFIPaBrwgRkaj (Fundamentals of the stiffness method) eKmanmeFüa)ayBIrsRmab;viPaKrcnasm<½n§edayeRbIviFIm:aRTIs. viFIPaBrwgRkajEdlRtUveRbI enAkñúgemeronenH nigemeroneRkayCakarviPaKedayeRbIviFIbMlas;TI. viFIkmøaMg EdleKehAfaviFI flexibility ¬Edlerobrab;enAkñúgkfaxNÐ 10-1¦ k¾GaceRbIedIm,IviPaKrcnasm<½n§ b:uEnþviFIenHminRtUv)an bgðajenAkñúgesovePAenHeT. mUlehtucm,gKW eKGaceRbIviFIPaBrwgRkajsRmab;viPaKrcnasm<½n§kMNt; edaysþaTic nigrcnasm<½n§minkMNt;edaysþaTic cMENkÉviFI flexibility RtUvkardMeNIrkarepSgsRmab; krNInImYy²énkrNITaMgBIr. ehIyviFIPaBrwgRkajpþl;eGaybMlas;TI nigkmøaMgedaypÞal; cMENkÉ viFI flexibility minpþl;eGaybMlas;TIedaypÞal;eT. elIsBIenH eKmanPaBgayRsYlsresrrUbmnþ m:aRTIsEdlcaM)ac;sRmab;RbtþibtþikarkMuBüÚT½redayeRbIviFIPaBrwgRkaj ehIyenAeBleKeFVIvarYc eK GacviPaKeRKOgbgÁúMedaykMuBüÚT½ry:agmanRbsiT§PaB. karGnuvtþviFIPaBrwgRkajTamTarnUvkarbMEbkeRKOgbgÁúMCaes‘rIén finite elements ehIyeK RtUvkMNt;GtþsBaØaNeGaycMNuccugrbs;Ggát;Ca node. sRmab;karviPaK truss, finite element Ca Ggát;nImYy²EdlpSMCa truss ehIy node CatMN. eKRtUvkMNt;lkçN³kmøaMg nigbMlas;TIrbs;Ggát; nImYy² ehIyeKRtUveFVITMnak;TMngrvagkmøaMg nigbMlas;TIedayeRbIsmIkarlMnwgkmøaMgEdlsresrenA Rtg; node. bnÞab;mk eKerobcMTMnak;TMngTaMgenH ¬sRmab;rcnasm<½n§TaMgmUl¦ CaRkumbBa©ÚlKña EdleKeGayeQμaHfa structure stiffness matrix K. enAeBlEdleKbegáItm:aRTIsrYcehIy eKGac kMNt;bMlas;TIrbs; node sRmab;bnÞúkenAelIrcnasm<½n§. enAeBlEdleKsÁal;bMlas;TIrYcehIy eK GackMNt;kmøaMgkñúgrbs;eRKOgbgÁúMedayeRbITMnak;TMngrvagkmøaMg nigbMlas;TIsRmab;Ggát;. karviPaK truss edayeRbIviFIPaBrwgRkaj T.Chhay -464
  • 2. mhaviTüal½ysMNg;sIuvil viTüasßanCatiBhubec©keTskm<úCa munnwgbegáItdMeNIrkarsRmab;GnuvtþviFIPaBrwgRkaj CaCMhandMbUgeyIgcaM)ac;yl;dwgBIniym n½y nigeKalKMnitmYycMnYn³ karkMNt;GtþsBaØaNrbs;Ggát; nig node³ CMhanmYyénCMhandMbUgkñúgkarGnuvtþviFIPaBrwgRkaj KWkMNt;GtþsBaØaNGgát;rbs;rcnasm<½n§ nig node rbs;va. eyIgnwgkMNt;Ggát;edaybg;elxEdl B½T§CMuvijedaykaer ehIyelxEdlB½T§CMuvijedayrgVg;kMNt;eGay node. ehIy eKk¾RtUvkMNt;cugCit nigcugq¶ayrbs;Ggát;edayeRbIk,alRBYjEdlvacg¥úleTAcugq¶ay. ]TahrN_énkarkMNt;Ggát; node nigTisedAsMrab; truss RtUv)anbgðajenAkñúgrUbTI 14-1a. kUGredaenskl nigkUGredaenGgát;³ edaysarbnÞúk nigbMlas;TICaTMhMviucT½r enaHeKcaM)ac;RtUv begáItRbB½n§kUGredaenedIm,IkMNt;TisedArbs;vaeGay)anRtwmRtUv. enATIenH eyIgnwgeRbIRbB½n§kUGr edaenBIrRbePTepSgKña. RbB½n§kUGredaenskl b¤RbB½n§kUGredaenrcnasm<½n§ ¬ x, y ¦ RtUveRbIedIm,I kMNt;TisedAénbnÞúkxageRkA nigTisedAénbgÁúM;bMlas;TIenARtg; node ¬rUbTI 14-1a¦. RbB½n§kUGr edaentMbn; b¤RbB½n§kUGredaenGgát;RtUv)aneRbIsRmab;Ggát;nImYy²edIm,IkMNt;TisedAénbMlas;TI rbs;va nigkmøaMgkñúgrbs;va. RbB½n§enHRtUv)ankMNt;edayeRbIG½kS x' , y' CamYynwgKl;enARtg; node Cit ehIyG½kS x' latsn§wgeq<aHeTArk node q¶ay. ]TahrN_sRmab;Ggát; truss elx $ RtUv )anbgðajenAkñúgrUbTI 14-1b. PaBminkMNt;sIueNm:aTic³ dUckarerobrab;enAkñúgkfaxNÐ 11-1, degree of freedom Edlminman karTb;sRmab; truss CaGBaØatdMbUgénviFIbMlas;TI dUcenHeKRtUvEtkMNt;va. tamc,ab;TUeTA eKman degree of freedom b¤bMlas;TIEdlGacekItmancMnYnBIr sMrab;tMN (node). sRmab;karGnuvtþ degree of freedom nImYy²RtUv)ankMNt;enAelI truss edayeRbIelxkUd ¬EdlbgðajenARtg;tMN b¤ Truss analysis using the stiffness method T.Chhay -465
  • 3. Department of Civil Engineering NPIC node ¦ ehIyeKeRbI k,alRBYjedaysMGageTAelIkUGredaensklviC¢man. ]TahrN_ truss enAkñúgrUbTI 14-1a man degree of freedom cMnYn8 EdlRtUv)ankMNt;;edayelxkUdBIelx 1 dl; elx 8 dUcbgðaj. Truss enHminkMNt;edaysIueNm:aTicdWeRkTI5 edaysarbMlas;TIEdlGac ekItmanTaMg 8enH elx1 dl;elx5 CaGBaØat b¤ degree of freedom EdlminmankarTb; ehIyelx 6 dl;elx8Ca degree of freedom EdlmankarTb;. edaysarmankarTb; bMlas;TIenATIenHRtUvesμI sUnü. sRmab;karGnuvtþbnþbnÞab; eyIgeRbIelxkUdtUc²sRmab;sMKal;bMlas;TIEdleyIgminsÁal; ¬degree of freedom EdlminTb;¦ ehIyelxkUcFM²sRmab;sMKal;bMlas;TIEdlsÁal; ¬degree of freedom EdlTb;¦. mUlehtukñúgkareFVIEbbenH edIm,IgayRsYlerobcM structure stiffness matrix dUcenHeyIgnwgGackMNt;bMlas;TIEdlCaGBaØatedaypÞal;. eRkayeBleyIgbg;elxeGay truss ehIykMNt;elxkUd eyIgGacKNna structure stiffness matrix K. edIm,IeFVIEbbenH dMbUgeyIgRtUvbegáIt member stiffness matrix k’ sRmab; Ggát;nImYy²rbs; truss. eKeRbIm:aRTIsenHedIm,IbgáajTMnak;TMngrvagbnÞúk nigbMlas;TIrbs;Ggát; edayeRbIkUGredaentMbn;. edaysarGgát;TaMgGs;rbs; truss minmanTisdUcKña eyIgRtUvbMElgTMhM TaMgenHBIkUGredaentMbn; x' , y' eTACakUGredaenskl x, y edayeRbIm:aRTIsbMElgkmøaMg nig bMlas;TI (force and displacement transformation matrices). eRkaybegáItrYcehIy eyIgGac bMElgm:aRTIsPaBrwgRkajrbs;Ggát;BIkUGredaentMbn;eTACakUGredaenskl ehIybnÞab;mkpÁúMva edIm,IbegáItCam:aRTIsPaBrwgRkajrcnasm<½n§. edayeRbI K ¬dUckarbgðajxagelI¦ dMbUgeyIgGac kMNt;bMlas;TIrbs; node bnÞab;mkeyIgGackMNt;kmøaMgRbtikmμTMr nigcugeRkayKWkmøaMgkñúgrbs; Ggát;. eyIgnwgbegáItviFIenH. !$>@> m:aRTIsPaBrwgRkajrbs;Ggát; (Member stiffness matrix) enAkñúgkfaxNÐenH eyIgnwgbegáItm:aRTIsPaBrwgRkajsMrab;Ggát;eTalrbs; truss edayeRbI kUGredaentMbn; x' , y' dUcbgðajenAkñúgrUbTI 14-2. tYenAkñúgm:aRTIsenHCaTMnak;TMngrvagbnÞúk nig bMlas;TIsRmab;Ggát;. Ggát;rbs; truss Gacpøas;TI)anEttamG½kS x' rbs;vab:ueNÑaH edaysarbnÞúkGnuvtþtamTis enH. dUcenH eKGacmanbMlas;TIÉkraCüBIr. enAeBleKeGaycugCitrbs;Ggát;manbMlas;TIviC¢man karviPaK truss edayeRbIviFIPaBrwgRkaj T.Chhay -466
  • 4. mhaviTüal½ysMNg;sIuvil viTüasßanCatiBhubec©keTskm<úCa dN ehIycMENkÉcugq¶ayRtUv)anTb;edaysnøak; ¬rUbTI 14-2a¦ enaHkmøaMgEdlekItmanenARtg; cugrbs;Ggát;KW AE AE q' N = dN q' F = − dN L L cMNaMfa q' GviC¢manedaysarsßanPaBlMnwg vaRtUveFVIGMeBItamTisedAGviC¢man x' . dUcKña bMlas;TI F viC¢man d enARtg;cugq¶ayedaycugCitenAEtTb;edaysnøak; ¬rUbTI 14-2b¦ pþl;nUvkmøaMgkñúgGgát; F AE AE q' ' N = − dF q' ' F = dF L L edaykareFIVtRmYtpl ¬rUbTI 14-2c¦ kmøaMgers‘ultg;EdlbgáedaybMlas;TITaMgBI AE AE qN = dN − dF (14-1) L L AE AE qF = dF − dN (14-2) L L eKGacsresrsmIkarTMnak;TMngrvagbnÞúk nigkmøaMgkñúgTRmg;m:aRTIs*Ca ⎡q N ⎤ AE ⎡ 1 − 1⎤ ⎡d N ⎤ ⎢ q ⎥ = L ⎢− 1 1 ⎥ ⎢ d ⎥ ⎣ F⎦ ⎣ ⎦⎣ F ⎦ b¤ q = k ' d (14-3) Edl k ' = AE ⎡−11 −11⎤ L ⎢ ⎥ (14-4) ⎣ ⎦ m:aRTIs k ' RtUv)aneKeGayeQμaHfam:aRTIsPaBrwgRkajsRmab;Ggát; ehIyvamanTRmg;dUcKñasRmab; Ggát;nImYy²rbs; truss. tYTaMgbYnEdlbegáItCam:aRTIsenHRtUv)aneKeGayeQμaHfaemKuNT§iBl kRmajsRmab;Ggát; (member stiffness influence coefficient) k' . k' CakmøaMgenARtg;tMN i ij ij enAeBltMN j ekItmanbMlas;TImYyÉktþa. ]TahrN_ RbsinebI i = j = 1 enaH k ' CakmøaMgenA11 Rtg;cugCit enAeBlcugq¶ayRtUv)anTb;edaybgáb; ehIycugCitrgbMlas;TI d = 1 eBalKW N AE q N = k '11 = L dUcKña eKkMNt;kmøaMgenAcugq¶ayBI i = 2 / j =1 dUcenH AE q F = k ' 21 = − L tYTaMgBIrenHCaCYrQrTImYyrbs;m:aRTIsPaBrwgRkajGgát;. tamrebobdUcKña CYrQrTIBIrrbs;m:aRTIs enHCakmøaMgenAkñúgGgát;enAeBlcugq¶ayrbs;Ggát;rgbMlas;TIÉktþa. * ]bsm<½n§ A pþl;eGaynUvkarrMlwkBIm:aRTIs. Truss analysis using the stiffness method T.Chhay -467
  • 5. Department of Civil Engineering NPIC !$>#> m:aRTIsbMElgénbMlas;TI nigkmøaMg (Displacement and force transformation matrices) edaysar truss pSMeLIgedayGgát;eRcIn eyIgnwg begáItviFIsRmab;bMElgkmøaMgkñúgGgát; q nig bMlas;TI d EdlkMNt;enAkñúgkUGredaentMbn;eGayeTACakUGredaen skl. edIm,IPaBgayRsYl eyIgnwgBicarNakUGredaen sklviC¢man x manTisedAeTAsþaM ehIy y manTisedA eLIgelI. mMurvagG½kSskl x, y nigG½kStMbn; x' , y' RtUv)ankMNt;eday θ x ehIy θ y dUcbgðajenAkñúgrUbTI 14-3. eyIgnwgeRbI kUsIunUsénmMuTaMgenHenAkñúgkarviPaK m:aRTIsdUcteTA. eyIgtag λ x = cosθ x ehIy λ y = cosθ y . eKGackMNt;témøCaelxsRmab; λ x nig λ y y:aggayedayeRbIkMuBüÚT½r enAeBleKkMNt; kUGredaen x, y éncugCit N nigcugq¶ay F rbs; Ggát;rYcehIy. ]TahrN_ eKmanGgát; NF dUcbgðajenAkñúgrUbTI 14-4. enATIenH kUGredaenrbs; N nig F KW (x N , y N ) nig (x F , y F ) erogKña . dUcenH * xF − x N xF − xN λ x = cos θ x = = (14-5) L (x F − xN ) + (yF − y N ) 2 2 yF − yN yF − yN λ y = cos θ y = = (14-6) L (x F − xN ) + (yF − yN ) 2 2 * Kl;rbs;kUGredaenGacsßitenATINak¾)an eGayEtmanlkçN³gayRsYl. b:uEnþ CaTUeTA vaeRcInsßitenARtg;TItaMgNaEdl kUGredaenrbs; node TaMgGs;viC¢man dUcbgðajenAkñúgrUbTI 14-4. karviPaK truss edayeRbIviFIPaBrwgRkaj T.Chhay -468
  • 6. mhaviTüal½ysMNg;sIuvil viTüasßanCatiBhubec©keTskm<úCa sBaØanBVnþenAkñúgsmIkarTUeTATaMgenHnwgKitedaysV½yRbvtþisRmab;Ggát;EdlsßitenAkñúgkaRdg;NamYy rbs;bøg; xy . m:aRTIsbMElgbMlas;TI³ enAkñúgkUGredaenskl cugnImYy²rbs;Ggát;Gacman degree of freedom b¤ bMlas;TIÉkraCüBIr eBalKWtMN N man DN nig DN ¬rUbTI 14-5a nig 14-5b¦ ehIytMN N man x y D F nig DF ¬rUbTI 14-5c nig14-5d¦. eyIgnwgBicarNabMlas;TITaMgenHdac;edayELkBIKñaedIm,I x y kMNt;bgÁúMbMlas;TIrbs;vatambeNþayGgát;. enAeBlcugq¶ayRtUv)anTb;edaysnøak; ehIycugCitmanbM las;TItamkUGredaenskl DN ¬rUbTI 14-5a¦ bMlas;TI ¬kMhUcRTg;RTay¦ EdlRtUvKñatambeNþay x Ggát;KW DN cosθ x *. dUcKña bMlas;TI DN nwgeFVIeGayGgát;pøas;TI DN cosθ y tambeNþayG½kS x' x y y ¬rUbTI 14-5b¦. T§iBlénbMlas;TIsklTaMgeFVIeGayGgát;pøas;TI. d N = D N x cos θ x + D N y cos θ y tamrebobdUcKña bMlas;TIviC¢man DF nig DF erogKña EdlGnuvtþenARtg;cugq¶ay F cMENkÉcugCit x y RtUv)anTb;edaysnøak; ¬rUbTI 14-5c nig 14-5d¦ nwgeFVIeGayGgát;pøas;TI d F = D Fx cos θ x + D Fy cos θ y edayeGay λ x = cosθ x nig λ y = cosθ y CakUsIunUsR)ab;Tis (direction cosine) sRmab;Ggát; eyIg)an d N = DN x λ x + DN y λ y d F = DFx λ x + DFy λ y EdleKGacsresrvaCaTRmg;m:aRTIs ⎡ DN x ⎤ ⎢ ⎥ ⎡ d N ⎤ ⎡λ x λ y 0 0 ⎤ ⎢ D N y ⎥ ⎢d ⎥ = ⎢ 0 0 λ λ ⎥⎢ D ⎥ (14-7) ⎣ F⎦ ⎣ x y⎦ ⎢ x⎥ F ⎢ D Fy ⎥ ⎣ ⎦ * eKminKitBIbMEbMrYl θ x b¤ θ y edaysarvamantémøtUceBk. Truss analysis using the stiffness method T.Chhay -469
  • 7. Department of Civil Engineering NPIC b¤ d = TD (14-8) ⎡λ x λ y 0 0 ⎤ Edl T =⎢ ⎥ (14-9) ⎣ 0 0 λx λ y ⎦ BIkarbMEbkxagelI T bMElgBIbMlas;TI D kñúgkUGredaenskl x, y TaMgbYneGayeTACabMlas;TI d kñúg kUGredaentMbn; x' cMnYnBIr. dUcenH T Cam:aRTIsbMElgbMlas;TI. m:aRTIsbMElgkmøaMg³ BicarNakarGnuvtþkmøaMg q eTAelIcugCitrbs;Ggát; cMENkcugq¶ayRtUv)anTb; N edaysnøak; ¬rUbTI 14-6a¦. enATIenH bgÁúMkmøaMgsklrbs; q N enARtg; N KW Q N x = q N cos x Q N y = q N cos θ y dUcKña RbsinebI q F RtUv)anGnuvtþeTAelIr)ar ¬rUbTI 14-6b¦ bgÁúMkmøaMgsklenARtg; F KW Q Fx = q F cos θ x Q Fy = q F cos θ y edayeRbIkUsIunUsR)ab;Tis λ x = cosθ x / λ y = cosθ y smIkarTaMgenHkøayCa QN x = q N λ x QN y = q N λ y Q Fx = q F λ x Q Fy = q F λ y EdleKGacsresrvaCaTRmg;m:aRTIsdUcxageRkam karviPaK truss edayeRbIviFIPaBrwgRkaj T.Chhay -470
  • 8. mhaviTüal½ysMNg;sIuvil viTüasßanCatiBhubec©keTskm<úCa ⎡Q N x ⎤ ⎡ λ x 0⎤ ⎢Q ⎥ ⎢ ⎥ ⎢ N y ⎥ = ⎢λ y 0⎥ ⎡q N ⎤ λx ⎥ ⎢qF ⎥ (14-10) ⎢ QFx ⎥ ⎢ 0 ⎣ ⎦ ⎢ ⎥ ⎢ ⎥ ⎢ Q Fy ⎥ ⎢ 0 ⎣ ⎦ ⎣ λy ⎥ ⎦ b¤ Q =TTq (14-11) ⎡λ x 0⎤ ⎢λ 0⎥ Edl TT =⎢ ⎢0 y ⎥ λx ⎥ (14-12) ⎢ ⎥ ⎢0 ⎣ λy ⎥ ⎦ enAkñúgkrNIenH T T bMElgBIkmøaMg q EdlmanGMeBIenARtg;cugrbs;Ggát;kñúgkUGredaentMbn; x' eGayeTA CakmøaMg Q EdlmanbgÁúMbYnkñúgkUGredaenskl x, y . tamkareRbobeFob m:aRTIsbMElgkmøaMgCa m:aRTIs transpose énm:aRTIsbMElgbMlas;TI ¬smIkar 14-9¦. !$>$> m:aRTIsPaBrwgRkajrbs;Ggát;kñúgkUGredaenskl (Member global stiffness matrix) eyIgnwgpþúMlT§plenAkñúgkfaxNÐxagelI ehIykMNt;m:aRTIsPaBrwgRkajsRmab;Ggát;EdlTak; TgnwgbgÁúMkmøaMgskl Q nigbMlas;TIskl D rbs;Ggát;. RbsinebIeyIgCMnYssmIkar 14-8 ¬ d = TD ¦ eTAkñúgsmIkar 14-3 ¬ q = k ' d ¦ eyIgGackMNt;kmøaMg q rbs;Ggát;CaGnuKmn_énbMlas;TIskl D enA Rtg;cMNuccugrbs;va eBalKW q = k ' TD (14-13) edayCMnYssmIkarenHeTAkñúgsmIkar 14-11 ¬ Q = T T q ¦ enaHeyIgnwgTTYl)anlT§plcugeRkay Q = T T k ' TD b¤ Q = KD (14-14) Truss analysis using the stiffness method T.Chhay -471
  • 9. Department of Civil Engineering NPIC Edk k = T T k 'T (14-15) m:aRTIs k Cam:aRTIsPaBrwgRkajsRmab;Ggát;enAkñúgkUGredaenskl. edaysareKsÁal; T T / T nig k ' enaHeyIg)an ⎡λ x 0⎤ ⎢λ 0 ⎥ AE ⎡ 1 − 1⎤ ⎡λ x λ y 0 0 ⎤ k=⎢ ⎥ y ⎢0 λ x ⎥ L ⎢− 1 1 ⎥ ⎢ 0 0 λ x λ y ⎥ ⎣ ⎦⎣ ⎦ ⎢ ⎥ ⎢0 ⎣ λy ⎥⎦ edayKNnaedaHRsaym:aRTIsxagelI eyIg)an Nx Ny Fx Fy ⎡ λ2 x λxλ y − λ2 x − λxλ y ⎤ N x AE ⎢ ⎥ k= ⎢ λx λ y λ2 y − λxλ y − λ2 ⎥ N y y (14-16) L ⎢ ⎢ − λx 2 − λxλ y λ2 x λ x λ y ⎥ Fx ⎥ ⎢− λ x λ y − λ2 λxλ y 2 ⎥F λy ⎦ y ⎣ y TItaMgrbs;tYnImYy³enAkñúgm:aRTIssIuemRTITMhM 4 × 4 tMNageGay degree of freedom sklnImYy²Edl pSMCamYynwgcugCit N nigCamYynwgcugq¶ay F . vaRtUv)anbgðajedaynimitþsBaØénelxkUdEdlenAtam CYredk nigCYrQr eBalKW N x , N y , Fx , Fy . enATIenH k CaTMnak;TMngrvagkmøaMg nigbMlas;TIsRmab; Ggát;enAeBlEdlbgÁúMénkmøaMg nigbMlas;TIenAcugrbs;Ggát;sßitenAkñúgkUGredaenskl b¤G½kS x, y . dUc enHtYnImYy²enAkñúgm:aRTIsCaemKuNT§iBlPaBrwgRkaj (stiffness influence coefficient) K ij Edl bgðajbgÁúMkmøaMg x b¤ y enARtg; i EdlcaM)ac;edIm,IeFVIeGaymanbgÁúMbMlas;TIÉktþa x b¤ y enARtg; j . Ca lT§pl CYrQrnImYy²rbs;m:aRTIstMNageGaybgÁúMkmøaMgbYnEdlekItmanenARtg;cugrbs;Ggát;enAeBl cugGgát;rgbMlas;TIÉktþaEdlTak;TgnwgCYrQrebs;m:aRTIsenaH. ]TahrN_ bMlas;TIÉktþa DN = 1 x nwgbegáItbgÁúMkmøaMgbYnenAelIGgát;EdlbgðajenAkñúgCYrQrTImYyrbs;m:aRTIs. !$>%> ma:RTIsPaBrwgRkajsMrab; truss (Truss stiffness matrix) eRkayeBlbegáItm:aRTIsPaBrwgRkajsRmab;Ggát;enAkñúgkUGredaensklrYcehIy eKcaM)ac;pÁúMBUk vabBa©ÚlKñatamlMdab;d¾RtwmRtUv dUcenHeKnwgTTYl)anm:aRTIsPaBrwgRkaj K sRmab; truss TaMgmUl. dM- eNIrkarénkarpÁúMm:aRTIsGgát;TaMgenHGaRs½ynwgkarkMNt;GtþsBaØaNrbs;Ggát;enAkñúgm:aRTIsGgát;nImYy ². dUckarerobrab;enAkñúgkfaxNÐmun eKRtUvtMerobCYredk nigCYrQrrbs;m:aRTIsedayelxkUdbYn N x , N y , Fx , Fy EdleRbIedIm,IkMNt;GtþsBaØaN degree of freedom sklBIrEdlGacekItmanenARtg; cugnImYy²rbs;Ggát; ¬emIlsmIkar 14-16¦. m:aRTIsPaBrwgRkajsRmab;eRKOgbgÁúMnwgmanlMdab;esμInwg karviPaK truss edayeRbIviFIPaBrwgRkaj T.Chhay -472
  • 10. mhaviTüal½ysMNg;sIuvil viTüasßanCatiBhubec©keTskm<úCa elxkUdx<s;bMputEdl)ankMNt;eTAelI truss edaysartMNageGaycMnYn degree of freedom srub sRmab;eRKOgbgÁúM. enAeBleKpÁúMm:aRTIs k eKRtUvCMnYstYnImYy²enAkñúg k eTAkñúgCYredk nigCYrQrRtUvKña rbs;m:aRTIsPaBrwgRkajsRmab;rcnasm<½n§ K . enAeBlGgát;BIr b¤Ggát;eRcIntP¢ab;KñaenARtg;tMNEtmYy eKRtUvdak;tYénm:aRTIsrbs;Ggát; k xøHeTAkñúgTItaMgdEdlrbs;m:aRTIs K . eKRtUvbUkbBa©ÚlKñatamlkçN³ nBVnþnUvtYEdlsßitenAkñúgTItaMgdUcKña. eyIgnwgyl;BImUlehtuenH)anc,as; RbsinebIeyIgdwgfatYnImYy² rbs;m:aRTIs k CaersIusþg;rbs;Ggát;Tb;Tl;nwgkmøaMgxageRkAEdlGnuvtþenARtg;cugrbs;va. tamviFIEbb enH karbUkbBa©ÚlKñanUversIusþg;tamTis x nigTis y enAeBlbegáItm:aRTIs K kMNt;nUversIusþg;srubrbs; tMNnImYy²EdlTb;Tl;nwgbMlas;TIÉktþatamTis x b¤tamTis y . ]TahrN_CaelxcMnYnBIrnwgbgðajBIviFIénkarpÁúMm:aRTIssRmab;Ggát;edIm,IbegáItCam:aRTIsPaBrwg RkajsRmab;eRKOgbgÁúM. eTaHbIvadMeNIrkarmanlkçN³sμúKsμajsRmab;karKNnaedayédbnþic Etvaman lkçN³gayRsYlCagsMrab;karbegáItkmμviFIenAelIkMuBüÚT½r. ]TahrN_ 14-1³ kMNt;m:aRTIsPaBrwgRkajsRmab; truss EdlmanGgát;BIrdUcbgðajenAkñúgrUbTI 14-7a. AE mantémøefr. dMeNaHRsay³ tamkarGegát ②manbgÁúMbMlas;TIEdlCaGBaØatcMnYnBIr cMENkÉ ① nig③RtUv)anTb; mineGaymanbMlas;TI. Cavi)ak eKRtUvkMNt;elxkUdeGaybgÁúMbMlas;TIenARtg;tMN ② dMbUgeK ehIy bnþedaytMN ③ nig ① ¬rUbTI14-7b¦. eKalrbs;RbB½n§kUGredaensklGacsßitenAcMNucNak¾)an. edIm,IPaBgayRsYl eyIgnwgeRCIserIstMN ② dUcbgðaj. eyIgGackMNt;elxerogeGayGgát;tam rebobNak¾)an ehIyeKRtUvKUssBaØaRBYjtambeNÞayGgát;TaMgBIredIm,IeGaydwgcugCit nigcugq¶ay bs;Ggát;nImYy². eKGacKNnakUsIunUsR)ab;Tis nigm:aRTIsPaBrwgRkajsRmab;Ggát;nImYy². Truss analysis using the stiffness method T.Chhay -473
  • 11. Department of Civil Engineering NPIC Ggát;elx1³ edaysar ②CacugCit ehIy ③Cacugq¶ay enaHtamsmIkar14-5 nig14-6 eyIg)an 3−0 0−0 λx = =1 λy = =0 3 3 edayeRbIsmIkar 14-16 nigedayEcktYnImYy²CamYynwg L = 3m eyIg)an 1 2 3 4 ⎡ 0.333 0 − 0.333 0⎤ 1 ⎢ 0⎥ 2 k1 = AE ⎢ 0 0 0 ⎥ ⎢− 0.333 0 0.333 0⎥ 3 ⎢ ⎥ ⎣ 0 0 0 0⎦ 4 eyIgGacRtYtBinitükarKNnaedaycMNaMfa k1 Cam:aRTIssIuemRTI. cMNaMfa CYredk nigCYrQrenAkñúg m:aRTIs k1 RtUv)ankMNt;eday degree of freedom x, y enAcugCit Edlbnþedaycugq¶ay eBalKW 1, 2, 3 nig 4 erogKña sRmab;Ggát;elx1 ¬rUbTI 14-7b¦. eKeFVIEbbenHedIm,IkMNt;tYsRmab;karpÁúMenAkñúg m:aRTIs K . Ggát;elx 2³ edaysar ②CacugCit ehIy ①Cacugq¶ay enaHeyIg)an 3−0 4−0 λx = = 0.6 λy = = 0.8 5 3 dUcenHsmIkar 14-16 CamYynwg L = 5m køayCa 1 2 5 6 ⎡ 0.072 0.096 − 0.072 − 0.096⎤ 1 ⎢ 0.128 − 0.096 − 0.128⎥ 2 k 2 = AE ⎢ 0.096 ⎥ ⎢− 0.072 − 0.096 0.072 0.096 ⎥ 5 ⎢ ⎥ ⎣− 0.096 − 0.128 0.096 0.128 ⎦ 6 enATIenH eKkMNt;CYredk nigCYrQrCa1, 2, 5 nig 6 edaysarelxTaMgenHtMNageGay degree of freedom tamTis x nig y enARtg;cugCit nigcugq¶ayrbs;Ggát;elx 2 . m:aRTIsPaBrwgRkajsRmab;rcnasm<½n§³ vaCam:aRTIsTMhM 6 × 6 edaysarvaman degree of freedom sRmab; truss cMnYn 6 ¬rUbTI 14-7b¦. eKRtUvbUktYEdlRtUvKñaénm:aRTIsTaMgBIrxagelIedIm,IbegáItCa m:aRTIsPaBrwgRkajsRmab;eRKOgbgÁúM. eKRbEhlCaRsYlemIlCagRbsinebIeKBnøatm:aRTIs k1 nig k 2 eGayeTACam:aRTIs 6 × 6 . enaHeK)an K = k1 + k 2 karviPaK truss edayeRbIviFIPaBrwgRkaj T.Chhay -474
  • 12. mhaviTüal½ysMNg;sIuvil viTüasßanCatiBhubec©keTskm<úCa 1 2 3 4 5 6 1 2 3 4 5 6 ⎡ 0.333 0 − 0.333 0 0 0⎤ 1 ⎡ 0.072 0.096 0 0 − 0.072 − 0.096⎤ 1 ⎢ 0 0 0 0 0 ⎥ 0⎥ 2 ⎢ 0.096 0.128 0 0 − 0.096 − 0.128⎥ 2 ⎢ ⎢ ⎥ K = AE ⎢− 0.333 0 0.333 0 0 0⎥ 3 + AE ⎢ 0 0 0 0 0 0 ⎥3 ⎢ ⎥ ⎢ ⎥ ⎢ 0 0 0 0 0 0⎥ 4 ⎢ 0 0 0 0 0 0 ⎥4 ⎢ 0 0 0 0 0 0⎥ 5 ⎢− 0.072 − 0.096 0 0 0.072 0.096 ⎥ 5 ⎢ ⎥ ⎢ ⎥ ⎢ 0 ⎣ 0 0 0 0 0⎥ 6 ⎦ ⎢− 0.096 − 0.128 ⎣ 0 0 0.096 0.128 ⎥ 6 ⎦ ⎡ 0.405 0.096 − 0.333 0 − 0.072 − 0.096⎤ ⎢ 0.096 0.128 0 0 − 0.096 − 0.128⎥ ⎢ ⎥ K = AE ⎢ − 0.333 0 0.333 0 0 0 ⎥ ⎢ ⎥ ⎢ 0 0 0 0 0 0 ⎥ ⎢− 0.072 − 0.096 0 0 0.072 0.096 ⎥ ⎢ ⎥ ⎢− 0.096 − 0.128 ⎣ 0 0 0.096 0.128 ⎥ ⎦ RbsinebIeKeFVIdMeNIrkarenHCamYynwgkMuBüÚT½r CaTUeTAeKcab;epþImCamYynwgm:aRTIs K EdlmanFatuTaMg Gs;esμIsUnü bnÞab;mkFatuénm:aRTIsPaBrwgRkajsklsRmab;Ggát;Edl)anKNnarYcehIyRtUv)anCMnYs edaypÞal;eTAkñúgTItaMgFatuEdlRtUvKñaénm:aRTIs K . kareFVIEbbenHvaRbesIrCagkarbegáItm:aRTIsPaBrwg RkajsRmab;Ggát; rUcehIyrkSavaTuk bnÞab;mkeTIbpÁúMva. ]TahrN_ 14-2³ kMNt;m:aRTIsPaBrwgRkajsRmab; truss EdlmanGgát;BIrdUcbgðajenAkñúgrUbTI 14-8a. AE mantémøefr. dMeNaHRsay³ eTaHbICa truss Carcnasm<½n§minkMNt;edaysþaTicdWeRkTImYyk¾eday Etvanwgminbgðaj BIPaBlM)akkñúgkarTTYl)anm:aRTIsPaBrwgRkajsRmab;rcnasm<½n§eT. eKkMNt;elxerogeGaytMN nig Truss analysis using the stiffness method T.Chhay -475
  • 13. Department of Civil Engineering NPIC Ggát;nImYy² ehIyeKbgðajcugCit nigcugq¶ayedayRBYjtambeNþayGgát;. dUcbgðajenAkñúgrUbTI 14- 8b dMbUgeKkMNt;elxerogkUdeGaybMlas;TIEdlminRtUv)anTb;. eKman degree of freedom cMnUn 8 dUcenH K RtUvCam:aRTIsTMhM 8 × 8 . edIm,IrkSaeGaykUGredaenrbs;tMNTaMgGs;viC¢man eKRtUveRCIserIs eKalrbs;kUGredaensklenARtg; ①. eyIgnwgGnuvtþsmIkar 14-5, 14-6 nig 14-16 eTAelIGgát; nImYy². Ggát;elx 1³ enATIenH L = 10m eyIg)an 10 − 0 0−0 λx = =1 λy = =0 10 10 1 2 6 5 ⎡ 0.1 0 − 0.1 0⎤ 1 ⎢ 0⎥ 2 k1 = AE ⎢ 0 0 0 ⎥ ⎢− 0.1 0 1 0⎥ 6 ⎢ ⎥ ⎣ 0 0 0 0⎦ 5 Ggát;elx 2³ enATIenH L = 10 2m dUcenH 10 − 0 10 − 0 λx = = 0.707 λy = = 0.707 10 2 10 2 1 2 7 8 ⎡ 0.035 0.035 − 0.035 − 0.035⎤ 1 ⎢ 0.035 0.035 − 0.035 − 0.035⎥ 2 k 2 = AE ⎢ ⎥ ⎢− 0.035 − 0.035 0.035 0.035 ⎥ 7 ⎢ ⎥ ⎣− 0.035 − 0.035 0.035 0.035 ⎦ 8 Ggát;elx 3³ enATIenH L = 10m dUcenH 0−0 10 − 0 λx = =0 λy = =1 10 10 1 2 3 4 ⎡0 0 0 0 ⎤1 ⎢0 0.1 0 − 0.1⎥ 2 k 3 = AE ⎢ ⎥ ⎢0 0 0 0 ⎥3 ⎢ ⎥ ⎣0 − 0.1 0 0.1 ⎦ 4 Ggát;elx 4³ enATIenH L = 10m eyIg)an 10 − 0 0−0 λx = =1 λy = =0 10 10 3 4 7 8 ⎡ 0.1 0 − 0.1 0⎤ 3 ⎢ 0⎥ 4 k 4 = AE ⎢ 0 0 0 ⎥ ⎢− 0.1 0 1 0⎥ 7 ⎢ ⎥ ⎣ 0 0 0 0⎦ 8 karviPaK truss edayeRbIviFIPaBrwgRkaj T.Chhay -476
  • 14. mhaviTüal½ysMNg;sIuvil viTüasßanCatiBhubec©keTskm<úCa Ggát;elx 5³ enATIenH L = 10 2m dUcenH 10 − 0 0 − 10 λx = = 0.707 λy = = −0.707 10 2 10 2 3 4 6 5 ⎡ 0.035 − 0.035 − 0.035 0.035 ⎤ 3 ⎢ 0.035 − 0.035⎥ 4 k 5 = AE ⎢− 0.035 0.035 ⎥ ⎢− 0.035 0.035 0.035 − 0.035⎥ 6 ⎢ ⎥ ⎣ 0.035 − 0.035 − 0.035 0.035 ⎦ 5 Ggát;elx 3³ enATIenH L = 10m dUcenH 0−0 10 − 0 λx = =0 λy = =1 10 10 6 5 7 8 ⎡0 0 0 0 ⎤6 ⎢0 0.1 0 − 0.1⎥ 5 k 6 = AE ⎢ ⎥ ⎢0 0 0 0 ⎥7 ⎢ ⎥ ⎣0 − 0.1 0 0.1 ⎦ 8 m:aRTIsPaBrwgRkajsRmab;rcnasm<½n§³ eKGacpÁúMm:aRTIsTaMg 6 edIm,IbegáItm:aRTIsTMhM 8 × 8 edaykarbUk bBa©ÚlFatuEdlRtUvKña. ]TahrN_ edaysar (k11 )1 = AE (0.1) / (k11 )2 = AE (0.035) / (k11 )3 = (k11 )4 = (k11 )5 = (k11 )6 = 0 enaH K11 = AE (0.1 + 0.035) = AE (0.135) . dUcenHlT§plcugeRkayKW 1 3 2 4 5 6 7 8 ⎡ 0.135 0 0.0350 0 − 0.1 − 0.035 − 0.035⎤ 1 ⎢ 0.035 0 − 0.1 0.135 0 0 − 0.035 − 0.035⎥ 2 ⎢ ⎥ ⎢ 0 0.135 − 0.035 0.035 − 0.035 − 0.1 0 0 ⎥3 ⎢ ⎥ K = AE ⎢ 0 − 0.035 0.135 − 0.035 0.035 − 0.1 0 0 ⎥4 ⎢ 0 0 0.035 − 0.035 0.135 − 0.035 0 − 0.1 ⎥ 5 ⎢ ⎥ ⎢ − 0.1 0 − 0.035 0.035 − 0.035 0.135 0 0 ⎥6 ⎢− 0.035 − 0.035 − 0.1 0 0 0 0.135 0.035 ⎥ 7 ⎢ ⎥ ⎢− 0.035 − 0.035 ⎣ 0 0 − 0.1 0 0.135 0.135 ⎥ 8 ⎦ !$>^> karGnuvtþénviFIPaBrwgRkajsRmab;karviPaK truss (Application of the stiffness method for truss analysis) eRkayeBlbegáItm:aRTIsPaBrwgRkajsRmab;eRKOgbgÁúMrYcehIy eKGaceFVIeGaybgÁúMkmøaMgskl Q EdlmanGMeBIenAelI truss manTMnak;TMngeTAnwgbMlas;TIskl D rbs;vaedayeRbI Q = KD (14-17) Truss analysis using the stiffness method T.Chhay -477
  • 15. Department of Civil Engineering NPIC eKGacsMKal;smIkarenHCasmIkarPaBrwgRkajsRmab;rcnasm<½n§ (structure stiffness equation). edaysareyIgEtgEtkMNt;elxkUdtUcbMputedIm,IsmÁal; degree of freedom EdlminRtUv)anTb; dUcenH vaGnuBaØateGayeyIgGacbMEbksmIkarenHkñúgTRmg;dUcxageRkam ³ * ⎡Qk ⎤ ⎡ K11 K12 ⎤ ⎡ Du ⎤ ⎢Q ⎥ = ⎢ K ⎥⎢ ⎥ (14-18) ⎣ u ⎦ ⎣ 21 K 22 ⎦ ⎣ Dk ⎦ Edl bnÞúkxageRkA nigbMlas;TIEdleKsÁal;. enATIenH bnÞúkmanGMeBIenAelI truss CaEpñk Qk , Dk = mYyéncMeNaT ehIyCaTUeTAbMlas;TIesμIsUnüedaysarTMrRtUv)anTb; dUcCaTMrsnøak; b¤TMrkl;. Qu , Du = bnÞúk nigbMlas;TIEdlCaGBaØat. enATIenH bnÞúkCakmøaMgRbtikmμTMrEdleKminsÁal; ehIybMlas;TIKWsßitenARtg;tMNEdlminRtUv)anTb;tamTisNamYyeT. K = m:aRTIsPaBrwgRkajsRmab;rcnasm<½n§ EdlRtUv)anbMEbkedIm,IeGaycuHsRmugCamYynwg karbMEbkrbs; Q nig D . edayBnøatsmIkar 14-18 eyIg)an Qk = K11 Du + K12 Dk (14-19) Qu = K 21 Du + K 22 Dk (14-20) CaTUeTA Dk = 0 edaysarTMrminmanbMlas;TI. RbsinebIvaEbbenHEmn enaHsmIkar 14-19 køayCa Qk = K11 Du edaysarFatuenAkñúgm:aRTIs K11 CaersIusþg;srubenARtg;tMN truss edIm,ITb;Tl;bMlas;TIÉktþatamTI x b¤ y enaHsmIkarxagelICakarRbmUlpþúMnUvsmIkarlMnwgkmøaMgEdlGnuvtþeTAelItMNEdlbnÞúkxageRkA esμIsUnü b¤mantémøEdlsÁal; (Qk ) . edayedaHRsayrk Du eyIg)an Du = [K11 ]−1 Qk (14-21) BIsmIkarenH eyIgGacTTYl)andMeNaHRsayedaypÞal;sRmab;bMlas;TIEdlCaGBaØatTaMgGs; bnÞab;mk edayeRbIsmIkar 14-20 CamYynwg Dk = 0 eyIg)an Qu = K 21 Du (14-22) BIsmIkarxagelI eyIgGackMNt;kmøaMgRbtikmμTMr. eKGackMNt;kmøaMgkñúgrbs;Ggát;edayeRbIsmIkar 14-13 eBalKW q = k ' TD edayBnøatsmIkarenH eyIg)an * eyIgnwg)aneXIjBIviFIbMEbkenHenAkñúg]TahrN_xageRkam. karviPaK truss edayeRbIviFIPaBrwgRkaj T.Chhay -478
  • 16. mhaviTüal½ysMNg;sIuvil viTüasßanCatiBhubec©keTskm<úCa ⎡ DN x ⎤ ⎢ ⎥ ⎡q N ⎤ AE ⎡ 1 − 1⎤ ⎡λ x λ y 0 0 ⎤ ⎢ D Ny ⎥ ⎢ q ⎥ = L ⎢− 1 1 ⎥ ⎢ 0 0 λ λ y ⎥ ⎢ DFx ⎥ ⎣ F⎦ ⎣ ⎦⎣ x ⎦⎢ ⎥ ⎢ DFy ⎥ ⎣ ⎦ edaysar q N = −q F edIm,IsßanPaBlMnwg dUcenHeKRtUvkarkMNt;EtkmøaMgmYyb:ueNÑaHkñúgcMeNamkmøaMg TaMgBIr. enATIenH eyIgnwgkMNt; q F kmøaMgEdlGnuvtþkmøaMgTajeTAelIGgát; ¬rUbTI 14-6b¦. ⎡ DN x ⎤ ⎢D ⎥ qF = AE L [ − λx − λ y λx ] λy ⎢ y ⎥ N ⎢ DFx ⎥ (14-23) ⎢ ⎥ ⎢ D Fy ⎥ ⎣ ⎦ RbsinebIlT§plEdl)anBIkarKNnamantémøGviC¢man enaHGgát;rgkarsgát;. dMeNIrkarkñúgkarviPaK (Procedure for analysis) xageRkamCaCMhanEdlpþl;nUvmeFüa)aysRmab;kMNt;bMlas;TI nigkmøaMgRbtikmμTMrEdlCa GBaØatsRmab; truss edayeRbIviFIPaBrwgRkaj. kareFVIkMNt;sMKal;³ begáItRbB½n§kUGredaenskl x, y . CaTUeTAeKalrbs;vasßitenARtg;tMNNaEdleFVIeGay kUGredaensRmab;tMNdéTeTotviC¢man. kMNt;elxerogeGaytMN nigGgát;nImYy² ehIykMNt;cugCit nigcugq¶ayrbs;Ggát;nImYy² edayeRbITisedArbs;sBaØaRBYj Edlk,alRBYjeq<aHeTArkcugq¶ay. kMNt;elxkUdBIrenARtg;tMNnImYy² edayeRbIelxtUcbMputsRmab;sMKal; degree of freedom EdlminmanrgkarTb; cMENkelxFMbMputsRmab;sMKal; degree of freedom EdlmankarTb;. begáIt Dk nig Qk . m:aRTIsPaBrwgRkajsRmab;eRKOgbgÁúM³ sRmab;Ggát;nImYy² kMNt; λ x nig λ y ehIykMNt;m:aRTIsPaBrwgRkajsRmab;Ggát;edayeRbI smIkar 14-16. pÁúMm:aRTIsTaMgenHedIm,IbegáItm:aRTIsPaBrwgRkajsRmab; truss TaMgmUl dUckarBnül;enAkñúg kfaxNÐ 14-5. edaykarRtYtBinitükarKNnaedayEpñk m:aRTIsPaBrwgRkajsRmab;Ggát; nig m:aRTIsPaBrwgRkajsRmab;rcnasm<½n§RtUvEtCam:aRTIssIuemRTI. bMlas;TI nigbnÞúk³ Truss analysis using the stiffness method T.Chhay -479
  • 17. Department of Civil Engineering NPIC bMEbkm:aRTIsPaBrwgRkajsRmab;rcnasm<½n§ dUcbgðajenAkñúgsmIkar 14-18. kMNt;bMlas;TIrbs;tMNEdlCaGBaØat Du edayeRbIsmIkar 14-21 kmøaMgRbtikmμTMr Qu eday eRbIsmIkar 14-22 ehIykmøaMgkñúgrbs;Ggát;nImYy² q F edayeRbIsmIkar 14-23. ]TahrN_ 14-3³ kMNt;kmøaMgkñúgrbs;Ggát;én truss EdlmanGgát;BIrdUcbgðajenAkñúgrUbTI 14-9a. AE mantémøefr. dMeNaHRsay³ kareFVIkMNt;smÁal;³ eKal x, y nigkarkMNt;elxerogrbs;tMN nigGgát;RtUv)anbgðajenAkñúgrUbTI 14-9b. dUcKña cugCit nigcugq¶ayRtUv)anbgðajkMNt;edaysBaØaRBYj ehIyeKeRbIelxkUdenARtg;tMN nImYy². tamkarGegáteyIgeXIjfabMlas;TI D3 = D4 = D5 = D6 = 0 . ehIybnÞúkxageRkAEdl eyIgsÁal;KW Q1 = 0, Q2 = −2kN . dUcenH ⎡0 ⎤ 3 ⎢0 ⎥ 4 ⎡ 0 ⎤1 Dk = ⎢ ⎥ Qk = ⎢ ⎥ ⎢0 ⎥ 5 ⎣ − 2⎦ 2 ⎢ ⎥ ⎣0 ⎦ 6 m:aRTIsPaBrwgRkajsRmab;rcnasm<½n§³ edayeRbIkareFVIkMNt;smÁal;dUcKña eyIgGacbegáItm:aRTIsPaBrwg RkajsRmab;rcnasm<½n§dUcbgðajenAkñúg]TahrN_ 14-1. bMlas;TI nigbnÞúk³ edaysresrsmIkar 14-17 ¬ Q = KD ¦ sRmab; truss eyIg)an karviPaK truss edayeRbIviFIPaBrwgRkaj T.Chhay -480
  • 18. mhaviTüal½ysMNg;sIuvil viTüasßanCatiBhubec©keTskm<úCa ⎡0 ⎤ ⎡ 0.405 0.096 − 0.333 0 − 0.072 − 0.096⎤ ⎡ D1 ⎤ ⎢ − 2⎥ ⎢ 0.096 0.128 0 0 − 0.096 − 0.128⎥ ⎢ D2 ⎥ ⎢ ⎥ ⎢ ⎥⎢ ⎥ ⎢ Q3 ⎥ ⎢ − 0.333 0 0.333 0 0 0 ⎥⎢ 0 ⎥ ⎢ ⎥ = AE ⎢ ⎥⎢ ⎥ (1) ⎢ Q4 ⎥ ⎢ 0 0 0 0 0 0 ⎥⎢ 0 ⎥ ⎢ Q5 ⎥ ⎢− 0.072 − 0.096 0 0 0.072 0.096 ⎥ ⎢ 0 ⎥ ⎢ ⎥ ⎢ ⎥⎢ ⎥ ⎢Q6 ⎥ ⎣ ⎦ ⎢− 0.096 − 0.128 ⎣ 0 0 0.096 0.128 ⎥ ⎢ 0 ⎥ ⎦⎣ ⎦ BIsmIkarenH eyIgGackMNt; K11 dUcenHeyIgGackMNt; Du . eyIgeXIjfaplKuNm:aRTIs ¬dUc smIkar 14-19¦ eyIg)an ⎡0 ⎤ ⎡0.405 0.096⎤ ⎡ D1 ⎤ ⎡0⎤ ⎢− 2⎥ = AE ⎢0.096 0.128⎥ ⎢ D ⎥ + ⎢0⎥ ⎣ ⎦ ⎣ ⎦⎣ 2 ⎦ ⎣ ⎦ enATIenH eyIgGacedaHRsayy:agRsYledayBnøatedaypÞal; 0 = AE (0.405 D1 + 0.096 D2 ) − 2 = AE (0.096 D1 + 0.128 D2 ) tamrUbviTüa smIkarTaMgenHtMNageGay ∑ Fx = 0 nig ∑ Fy = 0 EdlGnuvtþenARtg;tMN ②. eday edaHRsay eyIg)an 4.505 − 19.003 D1 = D2 = AE AE tamkarGegátrUbTI 14-9b eKrMBwgfatMN ②nwgpøas;TIeTAsþaM nigcuHeRkamdUcbgðajedaysBaØabUk nig sBaØadkéncemøIyenH edayeRbIlT§plTaMgenH eKGacTTYl)ankmøaMgRbtikmμTMrBIsmIkar (1) EdlRtUv)ansresrkñúgTRmg;én smIkar 14-20 ¬b¤smIkar 14-22¦ Ca ⎡Q3 ⎤ ⎡ − 0.333 0 ⎤ ⎡0 ⎤ ⎢Q ⎥ ⎢ 0 ⎥ 0 ⎥ 1 ⎡ 4.505 ⎤ ⎢0⎥ ⎢ 4 ⎥ = AE ⎢ +⎢ ⎥ ⎢Q5 ⎥ ⎢− 0.072 − 0.096⎥ AE ⎢− 19.003⎥ ⎢0⎥ ⎣ ⎦ ⎢ ⎥ ⎢ ⎥ ⎢ ⎥ ⎣Q6 ⎦ ⎣− 0.096 − 0.128⎦ ⎣0 ⎦ edayBnøat nigedaHRsaykmøaMgRbtikmμ Q3 = −0.333(4.505) = −1.5kN Q4 = 0 Q5 = −0.072(4.505) − 0.096(− 19.003) = 1.5kN Q6 = −0.096(4.505) − 0.128(− 19.003) = 2.0kN eKGacKNnakmøaMgenAkñúgGgát;nImYy²BIsmIkar 14-23. edayeRbITinñn½ysRmab; λ x nig λ y enAkñúg smIkar 14-1 eyIg)an Truss analysis using the stiffness method T.Chhay -481
  • 19. Department of Civil Engineering NPIC Ggát;elx ! ³ λ x = 1, λ y = 0, L = 3m ⎡ 4.505 ⎤ 1 ⎢ ⎥ AE 1 2 3 4 1 ⎢− 19.003⎥ 2 q1 = 3 [− 1 0 1 0] AE ⎢ 0 ⎥ 3 ⎢ ⎥ ⎣ 0 ⎦4 = [− 4.505] = −1.5kN 1 3 Ggát;elx @ ³ λ x = 0.6, λ y = 0.8, L = 5m ⎡ 4.505 ⎤ 1 AE 1 2 5 6 1 ⎢− 19.003⎥ 2 ⎢ ⎥ q2 = 5 [− 0.6 − 0.8 0.6 0.8] AE ⎢ 0 ⎥ 5 ⎢ ⎥ ⎣ 0 ⎦6 = [− 0.6(4.505) − 0.8(− 19.003)] = 2.5kN 1 5 Cak;EsþgeKGacepÞógpÞat;cemøIyTaMgenHedaysmIkarlMnwgEdlGnuvtþenARtg;tMN ②. ]TahrN_ 14-4³ kMNt;kmøaMgRbtikmμTMr nigkmøaMgkñúgrbs;Ggát;elx@ én truss dUcbgðajenAkñúgrUbTI 14-10a. AE mantémøefr. dMeNaHRsay³ kareFVIkMNt;smÁal;³tMN nigGgát;RtUv)ankMNt;elxerog ehIyeKalrbs;G½kS x, y RtUv)anbegáItenA Rtg;tMN ① ¬rUbTI 14-10b¦. ehIysBaØaRBYjRtUv)aneKeRbIedIm,IbgðajcugCit nigcugq¶ayrbs;Ggát; nImYy². edayeRbIelxkUd EdlelxtUcbMputtMNageGay degree of freedom EdlmanrgkarTb; ¬rUb TI 14-16b¦ eyIg)an karviPaK truss edayeRbIviFIPaBrwgRkaj T.Chhay -482
  • 20. mhaviTüal½ysMNg;sIuvil viTüasßanCatiBhubec©keTskm<úCa ⎡ 0 ⎤1 ⎢ 0 ⎥2 ⎡0 ⎤ 6 ⎢ ⎥ D k = ⎢0 ⎥ 7 ⎢ ⎥ Qk = ⎢ 2 ⎥ 3 ⎢ ⎥ ⎢0 ⎥ 8 ⎣ ⎦ ⎢ − 4⎥ 4 ⎢ 0 ⎥5 ⎣ ⎦ m:aRTIsPaBrwgRkajsRmab;rcnasm<½n§³ m:aRTIsenHRtUv)ankMNt;enAkñúg]TahrN_ 14-2 edayeRbIkar eFVIkMNt;smÁal;dUcKñanwgkarbgðajenAkñúg]TahrN_ 14-10b. bMlas;TI nigbnÞúk³ sRmab;cMeNaTenH Q = KD KW ⎡0⎤ ⎡ 0.135 0.035 0 0 0 − 0.1 − 0.035 − 0.035⎤ ⎡ D1 ⎤ ⎢0⎥ ⎢ 0.035 0.135 0 − 0 .1 0 0 − 0.035 − 0.035⎥ ⎢ D2 ⎥ ⎢ ⎥ ⎢ ⎥⎢ ⎥ ⎢ 2⎥ ⎢ 0 0 0.135 − 0.035 0.035 − 0.035 − 0.1 0 ⎥ ⎢ D3 ⎥ ⎢ ⎥ ⎢ ⎥⎢ ⎥ ⎢− 4⎥ = AE ⎢ 0 − 0.1 − 0.035 0.135 − 0.035 0.035 0 0 ⎥ ⎢ D4 ⎥ (1) ⎢0⎥ ⎢ 0 0 0.035 − 0.035 0.135 − 0.035 0 − 0.1 ⎥ ⎢ D5 ⎥ ⎢ ⎥ ⎢ ⎥⎢ ⎥ ⎢Q6 ⎥ ⎢ − 0 .1 0 − 0.035 0.035 − 0.035 0.135 0 0 ⎥⎢ 0 ⎥ ⎢Q ⎥ ⎢− 0.035 − 0.035 − 0.1 0 0 0 0.135 0.035 ⎥ ⎢ 0 ⎥ ⎢ 7⎥ ⎢ ⎥⎢ ⎥ ⎢ Q8 ⎥ ⎣ ⎦ ⎢− 0.035 − 0.035 ⎣ 0 0 − 0 .1 0 0.035 0.135 ⎥ ⎢ 0 ⎥ ⎦⎣ ⎦ edayeFVIplKuNdUckarsresrsmIkar 14-18 edIm,IedaHRsaybMlas;TI eyIg)an ⎡0 ⎤ ⎡0.135 0.035 0 0 0 ⎤ ⎡ D1 ⎤ ⎡0⎤ ⎢0 ⎥ ⎢ ⎥ ⎢0.035 0.135 ⎢ 0 − 0 .1 0 ⎥ ⎢ D2 ⎥ ⎢0 ⎥ ⎥⎢ ⎥ ⎢ ⎥ ⎢ 2 ⎥ = AE ⎢ 0 0 0.135 − 0.035 0.035 ⎥ ⎢ D3 ⎥ + ⎢0⎥ ⎢ ⎥ ⎢ ⎥⎢ ⎥ ⎢ ⎥ ⎢ − 4⎥ ⎢ 0 − 0.1 − 0.035 0.135 − 0.035⎥ ⎢ D4 ⎥ ⎢0⎥ ⎢0 ⎥ ⎣ ⎦ ⎢ 0 ⎣ 0 0.035 − 0.035 0.135 ⎥ ⎢ D5 ⎥ ⎢0⎥ ⎦⎣ ⎦ ⎣ ⎦ edayBnøat nigedayedaHRsaysmIkarsRmab;bMlas;TI eyIg)an ⎡ D1 ⎤ ⎡ 17.94 ⎤ ⎢D ⎥ ⎢− 69.20⎥ ⎢ 2⎥ 1 ⎢ ⎥ ⎢ D3 ⎥ = ⎢ − 2.06 ⎥ ⎢ ⎥ AE ⎢ ⎥ ⎢ D4 ⎥ ⎢ − 87.14 ⎥ ⎢ D5 ⎥ ⎣ ⎦ ⎢− 22.06⎥ ⎣ ⎦ edaybegáItsmIkar 14-20 BIsmIkar (1) EdleRbIlT§plEdl)anKNna eyIg)an ⎡ 17.94 ⎤ ⎢ − 69.20⎥ 0 ⎡Q6 ⎤ ⎡ − 0.1 0 − 0.035 0.035 − 0.035⎤ ⎥ ⎡ ⎤ ⎢Q ⎥ = AE ⎢− 0.035 − 0.035 − 0.1 1 ⎢ ⎢ 7⎥ ⎢ 0 0 ⎥ ⎥ ⎢ − 2.06 ⎥ + ⎢0⎥ AE ⎢ ⎥ ⎢ ⎥ ⎢ ⎥ ⎣Q8 ⎦ ⎢− 0.035 − 0.035 ⎣ 0 0 − 0.1 ⎥ ⎦ ⎢ − 87.14 ⎥ ⎢0⎥ ⎣ ⎦ ⎢− 22.06⎥ ⎣ ⎦ edayBnøat nigKNnakmøaMgRbtikmμTMr eyIg)an Truss analysis using the stiffness method T.Chhay -483
  • 21. Department of Civil Engineering NPIC Q6 = −4.0kN Q7 = 2.0kN Q8 = 4.0kN sBaØadksRmab; Q6 bgðajfakmøaMgRbtikmμrbs;TMrkl;eFVIGMeBIkñúgTis x GviC¢man. eKGackMNt;kmøaMg enAkñúgGgát;elx@ BIsmIkar 14-23 EdlBIsmIkar 14-2 λ x = 0.707, λ y = 0.707, L = 10 2m dUcenH ⎡ 17.94 ⎤ ⎢− 69.20⎥ q2 = AE [− 0.707 − 0.707 0.707 0.707] 1 ⎢ ⎥ 10 2 AE ⎢ 0 ⎥ ⎢ ⎥ ⎣ 0 ⎦ = 2.56kN ]TahrN_ 14-5³ kMNt;kmøaMgkñúgrbs;Ggát;elx@ énrcnasm<½n§dUcbgðajenAkñúgrUbTI 14-11a. Rb sinebIenARtg;tMN① mansMrut 25mm . yk AE = 8(103 )kN . dMeNaHRsay³ kareFVIkMNt;smÁal;³edIm,IPaBgayRsYl eKRtUvbegáIteKalrbs;kUGredaensklenARtg;tMN ③ dUc bgðajenAkñúgrUbTI 14-11b ehIytamFmμta eKeRbIelxkUdtUcCageKedIm,ItMNageGay degree of freedom EdlminmankarTb;. dUcenH ⎡ 0 ⎤3 ⎢− 0.025⎥ 4 ⎢ ⎥ ⎢ 0 ⎥5 ⎡0 ⎤ 1 Dk = ⎢ ⎥ Qk = ⎢ ⎥ ⎢ 0 ⎥6 ⎣0 ⎦ 2 ⎢ 0 ⎥7 ⎢ ⎥ ⎢ 0 ⎥8 ⎣ ⎦ karviPaK truss edayeRbIviFIPaBrwgRkaj T.Chhay -484
  • 22. mhaviTüal½ysMNg;sIuvil viTüasßanCatiBhubec©keTskm<úCa m:aRTIsPaBrwgRkajsRmab;rcnasm<½n§³ edayeRbIsmIkar 14-16 eyIg)an Ggát;elx !³ λ x = 0 / λ y = 1 / L = 3m dUcenH 3 4 1 2 ⎡0 0 0 0⎤3 ⎢0 0.333 0 − 0.333⎥ 4 k1 = AE ⎢ ⎥ ⎢0 0 0 0 ⎥1 ⎢ ⎥ ⎣0 − 0.333 0 0.333 ⎦ 2 Ggát;elx @³ λ x = −0.8, λ y = −0.6, L = 5m dUcenH 1 2 5 6 ⎡ 0.128 0.096 − 0.128 − 0.096⎤ 1 ⎢ 0.096 0.072 − 0.096 − 0.072⎥ 2 k 2 = AE ⎢ ⎥ ⎢ − 0.128 − 0.096 0.128 0.096 ⎥ 5 ⎢ ⎥ ⎣− 0.096 − 0.072 0.096 0.072 ⎦ 6 Ggát;elx #³ λ x = 1, λ y = 0, L = 4m dUcenH 7 8 1 2 ⎡ 0.25 0 − 0.25 0⎤ 7 ⎢ 0⎥ 8 k 3 = AE ⎢ 0 0 0 ⎥ ⎢− 0.25 0 0.25 0⎥ 1 ⎢ ⎥ ⎣ 0 0 0 0⎦ 2 edaypÁúMm:aRTIsTaMgenH m:aRTIsPaBrwgRkajsRmab;rcnasm<½n§køayCa 1 2 3 4 5 6 7 8 ⎡ 0.378 0.096 0 0 − 0.128 − 0.096 − 0.25 0⎤ 1 ⎢ 0.096 0.405 0 − 0.333 − 0.096 − 0.072 0 0⎥ 2 ⎢ ⎥ ⎢ 0 0 0 0 0 0 0 0⎥ 3 ⎢ ⎥ K =⎢ 0 − 0.333 0 0.333 0 0 0 0⎥ 4 ⎢ − 0.128 − 0.096 0 0 0.128 0.096 0 0⎥ 5 ⎢ ⎥ ⎢− 0.096 0.072 0 0 0.096 0.072 0 0⎥ 6 ⎢ − 0.25 0 0 0 0 0 0.25 0⎥ 7 ⎢ ⎥ ⎢ 0 ⎣ 0 0 0 0 0 0 0⎥ 8 ⎦ bMlas;TI nigbnÞúk³ enATIenH Q = KD eyIg)an Truss analysis using the stiffness method T.Chhay -485
  • 23. Department of Civil Engineering NPIC ⎡0⎤ ⎡ 0.378 0.096 0 0 − 0.128 − 0.096 − 0.25 0⎤ ⎡ D1 ⎤ ⎢0⎥ ⎢ 0.096 0.405 0 − 0.333 − 0.096 − 0.072 0 0 ⎥ ⎢ D2 ⎥ ⎢ ⎥ ⎢ ⎥⎢ ⎥ ⎢Q3 ⎥ ⎢ 0 0 0 0 0 0 0 0⎥ ⎢ 0 ⎥ ⎢ ⎥ ⎢ ⎥⎢ ⎥ ⎢Q4 ⎥ = AE ⎢ 0 − 0.333 0 0.333 0 0 0 0⎥ ⎢− 0.025⎥ ⎢Q5 ⎥ ⎢ − 0.128 − 0.096 0 0 0.128 0.096 0 0⎥ ⎢ 0 ⎥ ⎢ ⎥ ⎢ ⎥⎢ ⎥ ⎢Q6 ⎥ ⎢− 0.096 − 0.072 0 0 0.096 0.072 0 0⎥ ⎢ 0 ⎥ ⎢Q ⎥ ⎢ − 0.25 0 0 0 0 0 0.25 0⎥ ⎢ 0 ⎥ ⎢ 7⎥ ⎢ ⎥⎢ ⎥ ⎢Q8 ⎥ ⎣ ⎦ ⎢ 0 ⎣ 0 0 0 0 0 0 0⎥ ⎢ 0 ⎥ ⎦⎣ ⎦ edayedaHRsaysRmab;bMlas;TI ¬smIkar 14-19¦ eyIg)an ⎡ 0 ⎤ ⎢− 0.025⎥ ⎢ ⎥ ⎡0 ⎤ ⎡0.378 0.096⎤ ⎡ D1 ⎤ ⎡0 0 − 0.128 − 0.096 − 0.25 0⎤ ⎢ 0 ⎥ ⎢0⎥ = AE ⎢0.096 0.405⎥ ⎢ D ⎥ + AE ⎢0 − 0.333 − 0.096 − 0.072 ⎢ 0⎥ ⎢ 0 ⎥ ⎥ ⎣ ⎦ ⎣ ⎦⎣ 2 ⎦ ⎣ 0 ⎦ ⎢ 0 ⎥ ⎢ ⎥ ⎢ 0 ⎥ ⎣ ⎦ EdleyIgTTYl)an 0 = AE [(0.378 D1 + 0.096 D2 ) + 0] 0 = AE [(0.096 D1 + 0.405 D2 ) + 0.00833] edayedaHRsayRbB½n§smIkarenH eyIg)an D1 = 0.00556m D2 = −0.021875m eTaHbICaeKminRtUvkarKNnakmøaMgRbtikmμTMrk¾eday EtRbsinebIcaM)ac;eKRtUvKNnavaBIkarBnøatEdl kMNt;edaysmIkar 14-20. edayeRbIsmIkar 14-23 edIm,IkMNt;kmøaMgenAkñúgGgát;elx @ eyIg)an Ggát;elx @³ λ x = −0.8, λ y = −0.6, L = 5m, AE = 8(103 )kN dUcenH ⎡ 0.00556 ⎤ q2 = ( ) 8 10 3 [0.8 0.6 − 0.8 − 0.6]⎢ ⎢− 0.02187 ⎥ ⎥ 5 ⎢ 0 ⎥ ⎢ ⎥ ⎣ 0 ⎦ = 8 10( ) 3 (0.00444 − 0.0131) = −13.9kN 5 edayeRbIdMeNIrkarKNnadUcKña bgðajfakmøaMgenAkñúgGgát;elx ! KW q1 = 8.34kN ehIykmøaMgenAkñúg Ggát;elx # KW q3 = 11.1kN . lT§plRtUv)anbgðajenAkñúgdüaRkamGgÁesrIrbs;tMN ② ¬rUbTI 14- 11c¦ EdleKGacepÞógpÞat;edaysmIkarlMnwg. karviPaK truss edayeRbIviFIPaBrwgRkaj T.Chhay -486
  • 24. mhaviTüal½ysMNg;sIuvil viTüasßanCatiBhubec©keTskm<úCa !$>&> kUGredaenrbs; node (Nodal coordinates) enAeBlTMrkl;rbs; truss sßitenAelIbøg;eRTt ehIyeKGackMNt;PaBdabsUnüenARtg;TMreday eRbIRbB½n§kUGredaenskltamTisedk nigtamTisQrEtmYy. ]TahrN_ eKman truss enAkñúgrUbTI 14- 12a. eKRtUvkMNt;lkçxNÐénbMlas;TIsUnüenARtg;tMN ① tambeNþayG½kS y' ' ehIyedaysarTMr kl;Gacpøas;TItambeNþayG½kS x' ' dUcenH node enHRtUvmanbgÁúMbMlas;TItamG½kSkUGredaen x, y . sRmab;mUlehtuenH eyIgminGacrYmbBa©ÚllkçxNÐbMlas;TIsUnüenARtg; node enH enAeBlsresr smIkarPaBrwgRkajsklsRmab; truss edayeRbIG½kS x, y edaymineFVIeGaymankarEktRmUvdMeNIr karviPaKm:aRTIs. edIm,IedaHRsaycMeNaTenH eyIgGacbBa©ÚlvaeTAkñgkarviPaKkMuBüÚT½redayRsYl eyIgnwgeRbIsMnMu ú kUGredaenrbs; node x' ' , y' ' enARtg;TMreRTt. eKRtUveFVIeGayG½kSTaMgenHmanTItaMgy:agNaedIm,I eGaykmøaMgRbtikmμTMr nigbMlas;TIrbs;TMrpøas;TItambeNþayG½kSkUGredaennImYy² ¬rUbTI 14-12a¦. edIm,IKNnasmIkarPaBrwgRkajsklsRmab; truss enaHeKcaM)ac;begáItm:aRTIsbMElgkmøaMg nigma:RTIs bMElgbMlas;TIsRmab;Ggát;EdltP¢ab;eTAnwgTMrenaH dUcenHeKGaceFVIplbUklT§plTaMgenHenAkñúgRbB½n§ kUGredaenskl x, y dUcKña. edIm,IbgðajBIrebobénkarGnuvtþ eyIgRtUvBicarNaGgát; truss elx! enA Truss analysis using the stiffness method T.Chhay -487
  • 25. Department of Civil Engineering NPIC kñúgrUbTI 14-12b EdlmanRbB½n§kUGredaenskl x, y enARtg;cugCit N ehIyRbB½n§kUGredaenrbs; node x' ' , y ' ' enARtg;cugq¶ay F . enAeBlbMlas;TI D ekIteLIg dUcenHBYkvamanbgÁúMtambeNþayG½kS nImYy²dUcbgðajenAkñúgrUbTI 14-12c enaHbMlas;TItamTis x tambeNþaycugGgát;nImYy²køayCa d N = D N x cos θ x + D N y cos θ y d F = DFx '' cos θ x '' + DFy '' cos θ y '' eKGacsresrsmIkarTaMgenHenAkñúgTRmg;m:aRTIs ⎡ DN x ⎤ ⎢ ⎥ ⎡ d N ⎤ ⎡λ x λ y 0 0 ⎤ ⎢ DN y ⎥ ⎢d ⎥ = ⎢ 0 0 λ λ y '' ⎥ ⎢ DFx '' ⎥ ⎣ F⎦ ⎣ x '' ⎦⎢ ⎥ ⎢ D Fy '' ⎥ ⎣ ⎦ dUcKña kmøaMg q enARtg;cugCit nigcugq¶ayrbs;Ggát; ¬rUbTI 14-12d¦ manbgÁúM Q tambeNþayG½kSskl Q N x = q N cos θ x Q N y = q N cos θ y Q Fx '' = q F cos θ x '' Q Fy '' = q F cos θ y '' EdleKGacsresrCa ⎡ Q N x ⎤ ⎡λ x 0 ⎤ ⎢Q ⎥ ⎢ ⎥ ⎢ N y ⎥ = ⎢λ y 0 ⎥ ⎡ q N ⎤ ⎢Q Fx '' ⎥ ⎢ 0 λ x '' ⎥ ⎢ q F ⎥ ⎣ ⎦ ⎢ ⎥ ⎢ ⎥ ⎢Q Fy '' ⎥ ⎢ 0 λ y '' ⎥ ⎣ ⎦ ⎣ ⎦ eKeRbIm:aRTIsbMElgbMlas;TI nigm:aRTIskmøaMgenAkñúgsmIkarxagelIedIm,IbegáItm:aRTIsPaBrwgRkaj sRmab;Ggát;enAkñúgsßanPaBenH. edayGnuvtþsmIkar 14-15 eyIg)an k = T T k 'T ⎡λ x 0 ⎤ ⎢λ ⎥ k= ⎢ y 0 ⎥ AE ⎡ 1 − 1⎤ ⎡λ x λ y 0 0 ⎤ ⎢− 1 1 ⎥ ⎢ 0 0 λ ⎢ 0 λ x '' ⎥ L ⎣ ⎥ ⎦⎣ x '' λ y '' ⎦ ⎢ ⎥ ⎢ 0 λ y '' ⎥ ⎣ ⎦ edayKNnam:aRTIsxagelI eyIgTTYl)an ⎡ λ2 x λ x λ y − λ x λ x '' − λ x λ y '' ⎤ ⎢ ⎥ AE ⎢ λ x λ y λ2 y − λ y λ x '' − λ y λ y '' ⎥ k= (14-24) L ⎢ − λ x λ x '' − λ y λ x '' λ2 '' λ x '' λ y '' ⎥ ⎢ x ⎥ ⎢− λ x λ y '' − λ y λ y '' λ x '' λ y '' λ2 '' ⎥ ⎣ y ⎦ bnÞab;mkeKGaceRbIm:aRTIsPaBrwgRkajsRmab;Ggát;nImYy²EdlRtUvtP¢ab;eTAnwgTMrkl;EdleRTt ehIy dMeNIrkarpÁúMm:aRTIsedIm,IbegáItm:aRTIsPaBrwgRkajrcnasm<½n§GnuvtþtamdMeNIrkarbTdæan. ]TahrN_xag karviPaK truss edayeRbIviFIPaBrwgRkaj T.Chhay -488
  • 26. mhaviTüal½ysMNg;sIuvil viTüasßanCatiBhubec©keTskm<úCa eRkambgðajBIkarGnuvtþrbs;va. ]TahrN_ 14-6³ kMNt;kmøaMgRbtikmμTMrsRmab; truss dUcbgðajenAkñúgrUbTI 14-13a. dMeNaHRsay³ kareFVIkMNt;smÁal;³edaysarTMrkl;enARtg; ② sßitenAelIbøg;eRTt eyIgRtUveRbIkUGredaenrbs; node enARtg; node enH. eKRtUvkMNt;elxerogeGaytMN nigGgát; ehIybegáItkUGredaen x, y enARtg; node ③ ¬rUbTI 14-13b¦. cMNaMfa elxkUd # nig$ sßitenAtambeNþayG½kS x' ' , y ' ' edIm,IeRbIlkçxNÐ Edl D4 = 0 . m:aRTIsPaBrwgRkajsRmab;Ggát;³ eKRtUvbegáItm:aRTIsPaBrwgRkajsRmab;Ggát;elx ! nigelx @ eday eRbIsmIkar 14-24 edaysarGgát;TaMgenHmanelxkUdtamTisénG½kSskl nigG½kSrbs;kUd. eKRtUv kMNt;m:aRTIsPaBrwgRkajsRmab;Ggát;elx # tamrebobFmμta. Ggát;elx !³ rUbTI 14-13c/ λ x = 1, λ y = 0, λ x'' = 0.707, λ y'' = −0.707 Truss analysis using the stiffness method T.Chhay -489
  • 27. Department of Civil Engineering NPIC 5 6 3 4 ⎡ 0.25 0 − 0.17675 0.17675⎤ 5 ⎢ 0 ⎥6 k1 = AE ⎢ 0 0 0 ⎥ ⎢− 0.17675 0 0.125 − 0.125 ⎥ 3 ⎢ ⎥ ⎣ 0.17675 0 − 0.125 0.125 ⎦ 4 Ggát;elx @³ rUbTI 14-13d/ λ x = 0, λ y = −1, λ x '' = −0.707, λ y '' = −0.707 1 2 3 4 ⎡ 0 0 0 0 ⎤1 ⎢0 0.333 − 0.2357 − 0.2357⎥ k 2 = AE ⎢ ⎥2 ⎢0 − 0.2357 0.1667 0.1667 ⎥ 3 ⎢ ⎥ ⎣0 − 0.2357 0.1667 0.1667 ⎦ 4 Ggát;elx #³ λ x = 0.8, λ y = 0.6 1 2 3 4 ⎡ 0.128 0.096 − 0.128 − 0.096⎤ 5 ⎢ 0.096 0.072 − 0.0.96 − 0.072⎥ 6 k 3 = AE ⎢ ⎥ ⎢− 0.128 − 0.096 0.128 0.096 ⎥ 1 ⎢ ⎥ ⎣− 0.096 − 0.072 0.0.96 0.072 ⎦ 2 m:aRTIsPaBrwgRkajsRmab;rcnasm<½n§³ pÁúMm:aRTIsTaMgenHedIm,IkMNt;m:aRTIsPaBrwgRkajsRmab;rcna sm<½n§ eyIg)an ⎡ 30 ⎤ ⎡ 0.128 0.096 0 0 − 0.128 − 0.096⎤ ⎡ D1 ⎤ ⎢0⎥ ⎢ 0.096 0.4053 − 0.2357 − 0.2357 − 0.096 − 0.072⎥ ⎢ D2 ⎥ ⎢ ⎥ ⎢ ⎥⎢ ⎥ ⎢0⎥ ⎢ 0 − 0.2357 0.2917 0.0417 − 0.17675 0 ⎥ ⎢ D3 ⎥ ⎢ ⎥ = AE ⎢ ⎥⎢ ⎥ ⎢Q4 ⎥ ⎢ 0 − 0.2357 0.417 0.2917 0.17375 0 ⎥⎢ 0 ⎥ ⎢Q5 ⎥ ⎢ − 0.128 − 0.096 − 0.17675 0.17675 0.378 0.096 ⎥ ⎢ 0 ⎥ ⎢ ⎥ ⎢ ⎥⎢ ⎥ ⎢Q6 ⎥ ⎣ ⎦ ⎢− 0.096 − 0.072 ⎣ 0 0 0.096 0.072 ⎥ ⎢ 0 ⎥ ⎦⎣ ⎦ edayeFVIplKuNm:aRTIsénm:aRTIsEpñkxagelI enaHeyIgGackMNt;bMlas;TI D EdlCaGBaØatBIkaredaH RsayRbB½n§smIkar eBalKW 352.5 D1 = AE − 157.5 D2 = AE − 127.3 D3 = AE eKGacTTYl)ankmøaMgRbtikmμ Q BIplKuNm:aRTIsénm:aRTIsxageRkamenAkñúgsmIkar (1). edayeRbI bMlas;TIEdl)anKNna eyIg)an Q4 = 0(352.5) − 0.2357(− 157.5) + 0.0417(− 127.3) karviPaK truss edayeRbIviFIPaBrwgRkaj T.Chhay -490
  • 28. mhaviTüal½ysMNg;sIuvil viTüasßanCatiBhubec©keTskm<úCa = 31.8kN Q5 = −0.128(352.5) − 0.096(− 157.5) − 0.17675(− 127.3) = −7.5kN Q6 = −0.096(352.5) − 0.072(− 157.5) + 0(− 127.3) = −22.5kN !$>*> Trusses EdlmanbMErbMrYlsItuNðaPaB nigkMhusénplitkmμ (Truss having thermal changes and fabrication errors) RbsinebIGgát;xøHrbs; truss rgnUvkarlUt b¤rYjEdlbNþalBIbMErbMrYlsItuNðPaB b¤kMhusén plitkmμ enaHeKcaM)ac;RtUveRbIviFItRmYtpledIm,ITTYl)andMeNaHRsay. vaRtUvkarbICMhan. dMbUg eK caM)ac;RtUvKNnakmøaMgbgáb;cugEdlkarBarkarcl½trbs; node EdlbNþalBIsItuNðPaB b¤kMhusén plitkmμ. CMhanTIBIrKWeKRtUvdak;kmøaMgEdlesμIKña b:uEnþmanTispÞúyKñaenAelI truss Rtg; node ehIyeK RtUvKNnabMlas;TIrbs; node edayeRbIkarviPaKm:aRTIs. cugeRkay eKkMNt;kmøaMgCak;EsþgenAkñúg Ggát; nigkmøaMgRbtikmμenAelI truss edaykareFVItRmYtplénlT§plTaMgBIrenH. Cak;Esþg eKRtUvkar dMeNIrkarenH RbsinebI truss Carcnasm<½n§minkMNt;edaysþaTic. RbsinebI truss Carcnasm<½n§kMNt; edaysþaTic eKGackMNt;bMlas;TIenARtg; node edayviFIenH b:uEnþbMErbMrYlsItuNðPaB nigkMhusén plitkmμnwgminmanT§iBleTAelIkmøaMgRbtikmμ nigkmøaMgkñúgrbs;Ggát; edaysareKGacEktRmUvbERm bRmYlRbEvgrbs;Ggát; truss edayesrI. T§iBlkMedA³ RbsinebIGgát; truss manRbEvg L rgkMeNInsItuNðPaB ΔT RbEvgrbs;Ggát; nwgmankMhUcRTg;RTay ΔL = αΔTL Edl α Ca emKuNrIkedaysarkMedA. kmøaMgsgát; qo Edl GnuvtþeTAelIGgát;nwgeFVIeGayRbEvgrbs;Ggát; rYj)anRbEvg ΔL' = qo L / AE . RbsinebIeyIg dak;eGaybMlas;TITaMgBIresμIKña enaH qo = AEαΔT . kmøaMgenHnwgTb;Ggát;dUcbgðajenAkñúgrUbTI 14-14 dUcenHeyIg)an (q N )0 = AEαΔT (q F )0 = − AEαΔT Truss analysis using the stiffness method T.Chhay -491
  • 29. Department of Civil Engineering NPIC eKRtUvdwgfa RbsinekItmankarfykMedA enaH ΔT køayCaGviC¢man ehIykmøaMgTaMgenHnwgbRBa©asTisedA edIm,IeFVIeGayGgát;sßitenAkñúgsßanPaBlMnwg. eyIgGacbMElgkmøaMgTaMgBIrenHeTAkñúgkUGredaenskledayeRbIsmIkar 14-10 EdleFVIeGay ( ⎡ QN x )0 ⎤ ⎡λ x 0 ⎤ ⎡ λx ⎤ ( ) ⎢Q ⎢ Ny ⎥ ⎢ λ 0⎥ = ⎢ y 0⎥ ⎥ ⎡1⎤ ⎢λ ⎥ ⎢ y ⎥ ( ) ⎢ QF ⎥ ⎢ 0 λ x ⎥ AEαΔT ⎢− 1⎥ = AEαΔT ⎢ − λ x ⎥ ⎣ ⎦ (14-25) ( ) ⎢ x ⎢ Q Fy ⎣ 0⎥ 0⎥ ⎢ ⎦ ⎣ ⎢ ⎥ 0 λy ⎥ ⎦ ⎢ ⎢− λ y ⎥ ⎣ ⎥ ⎦ kMhusqÁgkñúgplitkmμ³ RbsinebIeKeFVIeGayGgát;EvgCaRbEvgedImedayTMhM ΔL muxeBlP¢ab;vaeTAnwg truss enaHkmøaMg qo EdlcaM)ac;edIm,IrkSaGgát;RtwmRbEvgDIsaj L KW qo = AEΔL / L dUcenHsRmab; Ggát;enAkñúgrUbTI 14-14 eyIg)an AEΔL (q N )0 = L AEΔL (q F )0 =− L RbsinebIGgát;enHxøICagRbEvgedIm enaH ΔL køayCaGviC¢man ehIykmøaMgTaMgenHnwgbRBa©as. enAkñúgkUGredaenskl kmøaMgTaMgenHKW ( ⎡ QN x )0 ⎤ ⎡ λx ⎤ ⎢Q( ) ⎢ Ny ⎥ ⎢λ ⎥ 0 ⎥ = AEΔL ⎢ y ⎥ ( ) ⎢ QF ⎥ L ⎢− λ x ⎥ (14-26) ( ) ⎢ x ⎢ Q Fy ⎣ 0⎥ 0⎦⎥ ⎢ ⎣ ⎥ ⎢− λ y ⎥ ⎦ karviPaKm:aRTIs³ enAkñúgkrNITUeTA CamYy truss rgkmøaMgGnuvtþ bERmbRmYlsItuNðPaB nigkMhusén plitkmμ TMnak;TMngrvagkmøaMgkñúg nigbMlas;TIsRmab; truss enaHvakøayCa Q = KD + Q0 (14-27) enATIenH Q0 Cam:aRTIsCYrQrsRmab; truss TaMgmUlrbs;kmøaMgbgáb;cugEdlbNþalBIbERmbRmYl sItuNðPaB nigkMhusénplitkmμrbs;Ggát;EdlkMNt;enAkñúgsmIkar 14-25 nig 14-26. eyIgGacEbg EcksmIkarenHenAkñúgTRmg;dUcxageRkam ⎡Qk ⎤ ⎡ K11 K12 ⎤ ⎡ Du ⎤ ⎡(Qk )0 ⎤ ⎢Q ⎥ = ⎢ K ⎥⎢ ⎥ + ⎢ ⎥ ⎣ u ⎦ ⎣ 21 K 22 ⎦ ⎣ Dk ⎦ ⎣(Qu )0 ⎦ edayedaHRsaym:aRTIsenAGgÁxagsþaM eyIgTTYl)an Qk = K11 Du + K 21 Dk + (Qk )0 (14-28) Qu = K 21 Du + K 22 Dk + (Qu )0 (14-29) karviPaK truss edayeRbIviFIPaBrwgRkaj T.Chhay -492
  • 30. mhaviTüal½ysMNg;sIuvil viTüasßanCatiBhubec©keTskm<úCa eyagtamdMeNIrkartRmYtplEdlerobrab;xagelI eyIgGackMNt;bMlas;TI Du BIsmIkarTImYyedaydk K12 Dk nig (Qk )0 BIGgÁTaMgBIr bnÞab;mkeyIgedaHRsay Du . eyIgTTYl)an Du = K111 (Qk − K12 Dk − (Qk )0 ) − eRkayeBleyIgTTYl)anbMlas;TIrbs; node enaHeyIgGackMNt;kmøaMgkñúgrbs;Ggát;edayviFItRmYtpl eBalKW q = k ' TD + q0 RbsinebIeyIgBnøatsmIkarenHedIm,IkMNt;kmøaMgenAcugq¶ayrbs;Ggát; eyIgTTYl)an ⎡ DN x ⎤ ⎢D ⎥ qF = AE L [ − λx − λ y λx ] λ y ⎢ y ⎥ − (q F )0 N ⎢ DFx ⎥ (14-30) ⎢ ⎥ ⎢ D Fy ⎥ ⎣ ⎦ lT§plenHRsedogKñaeTAnwgsmIkar 14-23 EtvaxusKñaRtg;enATIenHvamanplbUkéntY (q F )0 EdlCa kmøaMgbgáb;cugrbs;Ggát;EdlbNþalBIbERmbRmYlsItuNðPaB nig / b¤kMhusénplitkmμdUckMNt;dUcxag elI. eKRtUvdwgfa RbsinebIlT§plEdlTTYl)anBIsmIkarenHmantémøGviC¢man enaHGgát;nwgrgkmøaMg sgát;. ]TahrN_TaMgBIrxageRkam nwgbgðajBIkarGnuvtþéndMeNIrkarrbs;viFIenH. ]TahrN_ 14-7³ kMNt;kmøaMgkñúgGgát;elx ! nig elx @ rbs; truss EdlmanTMrsnøak;dUcbgðajenA kñúgrUbTI 14-15 RbsinebIeKeFVIeGayGgát;elx @ xøICagmun 0.01 munnwgpÁúMvaeTAkñúg truss. yk AE = 8(10 3 )kN . dMeNaHRsay³ edaysarGgát;manRbEvgxøI enaH ΔL = −0.01m dUcenHGnuvtþsmIkar 14-26 eTAelIGgát;elx @ CamYy nwg λ x = −0.8, λ y = −0.6 eyIg)an ⎡ (Q1 )0 ⎤ ⎡ − 0.8 ⎤ ⎡ 0.0016 ⎤ 1 ⎢(Q ) ⎥ ⎢ − 0.6 ⎥ ⎢ ⎥ ⎢ 2 0 ⎥ = AE (− 0.01) ⎢ ⎥ = AE ⎢ 0.0012 ⎥ 2 ⎢(Q5 )0 ⎥ 5 ⎢ 0.8 ⎥ ⎢− 0.0016⎥ 5 ⎢ ⎥ ⎢ ⎥ ⎢ ⎥ ⎢(Q6 )0 ⎥ ⎣ ⎦ ⎣ 0.6 ⎦ ⎣− 0.0012⎦ 6 Truss analysis using the stiffness method T.Chhay -493
  • 31. Department of Civil Engineering NPIC eK)anbegáItm:aRTIsPaBrwgRkajsRmab;rcnasm<n§enAkñúg]TahrN_ 14-4. edayGnuvtþsmIkar 14-27 ½ eyIg)an ⎡0⎤ ⎡ 0.378 0.096 0 0 − 0.128 − 0.096 − 0.25 0⎤ ⎡ D1 ⎤ ⎡ 0.0016 ⎤ ⎢0⎥ ⎢ 0.096 0.405 0 − 0.333 − 0.096 − 0.072 0 ⎥⎢D ⎥ 0⎥ ⎢ 2 ⎥ ⎢ 0.0012 ⎥ ⎢ ⎥ ⎢ ⎢ ⎥ ⎢Q3 ⎥ ⎢ 0 0 0 0 0 0 0 0⎥ ⎢ 0 ⎥ ⎢ 0 ⎥ ⎢ ⎥ ⎢ ⎥⎢ ⎥ ⎢ ⎥ ⎢Q4 ⎥ = AE ⎢ 0 − 0.333 0 0.333 0 0 0 0⎥ ⎢ 0 ⎥ ⎢ 0 ⎥ + AE ⎢Q5 ⎥ ⎢ − 0.128 − 0.096 0 0 0.128 0.096 0 0⎥ ⎢ 0 ⎥ ⎢− 0.0016⎥ ⎢ ⎥ ⎢ ⎥⎢ ⎥ ⎢ ⎥ ⎢Q6 ⎥ ⎢− 0.096 − 0.072 0 0 0.096 0.072 0 0⎥ ⎢ 0 ⎥ ⎢− 0.0012⎥ ⎢Q ⎥ ⎢ − 0.25 0 0 0 0 0 0.25 0⎥ ⎢ 0 ⎥ ⎢ 0 ⎥ ⎢ 7⎥ ⎢ ⎥⎢ ⎥ ⎢ ⎥ ⎢Q8 ⎥ ⎣ ⎦ ⎢ 0 ⎣ 0 0 0 0 0 0 0⎥ ⎢ 0 ⎥ ⎦⎣ ⎦ ⎢ ⎣ 0 ⎥ ⎦ edayEbgEckm:aRTIsenHdUcbgðaj nigedayedaHRsayplKuNm:aRTIsedIm,ITTYl)ansmIkarsRmab; bMlas;TI eyIgTTYl)an ⎡0⎤ ⎢0⎥ ⎢ ⎥ ⎡0 ⎤ ⎡0.378 0.096⎤ ⎡ D1 ⎤ ⎡0 0 − 0.128 − 0.096 − 0.25 0⎤ ⎢0⎥ ⎡0.0016⎤ ⎢0⎥ = AE ⎢0.096 0.405⎥ ⎢ D ⎥ + AE ⎢0 − 0.333 − 0.096 − 0.072 ⎥ ⎢0⎥ + AE ⎢0.0012⎥ ⎣ ⎦ ⎣ ⎦⎣ 2 ⎦ ⎣ 0 0⎦ ⎢ ⎥ ⎣ ⎦ ⎢0⎥ ⎢ ⎥ ⎢0⎥ ⎣ ⎦ EdleGay 0 = AE [0.378 D1 + 0.096 D2 ] + AE [0] + AE [0.0016] 0 = AE [0.096 D1 + 0.405 D2 ] + AE [0] + AE [0.0012] edaHRsayRbB½n§smIkar eyIgTTYl)an D1 = −0.003704m D2 = −0.002084m eTaHbICaminRtUvkar eKGackMNt;kmøaMgRbtikmμ Q BIkarBnøatsmIkar (1) EdlGnuvtþtamKMrUénsmIkar 14-29. edIm,IkMNt;kmøaMgenAkñúgGgát;elx ! nigelx @ eyIgRtUvGnuvtþsmIkar 14-30 EdlenAkñúgkrNI enH eyIg)an Ggát;elx !³ λ x = 0, λ y = 1, L = 3m, AE = 8(103 )kN dUcenH ⎡ 0 ⎤ q1 = ( ) 8 10 3 [0 − 1 0 1] ⎢ ⎢ 0 ⎥ ⎥ + [0] 3 ⎢− 0.003704⎥ ⎢ ⎥ ⎣− 0.002084⎦ karviPaK truss edayeRbIviFIPaBrwgRkaj T.Chhay -494
  • 32. mhaviTüal½ysMNg;sIuvil viTüasßanCatiBhubec©keTskm<úCa q1 = −5.56kN Ggát;elx @³ λ x = −0.8, ( ) dUcenH λ y = −0.6, L = 5m, AE = 8 10 3 kN ⎡− 0.003704⎤ q2 = ( ) 8 10 3 ⎢− 0.002084⎥ [0.8 0.6 − 0.8 − 0.6]⎢ ⎥ − 8 10 (− 0.01) 3 ( ) 5 ⎢ 0 ⎥ 5 ⎢ ⎥ ⎣ 0 ⎦ q 2 = 9.26kN ]TahrN_ 14-8³ Ggát;elx @ rbs; Edl truss bgðajenA kñúgrUbTI 14-16 rgnUvkMeNInsItuNðPaB 83.3o C . kMNt;kmøaMgEdlekItmanenAkñúgGgát;elx @. yk α = 11.7(10 −6 )/ o C / E = 200GPa . Ggát; nImYy²manRkLaépÞmuxkat; A = 484mm 2 . dMeNaHRsay³ edaysar vamankMeNInsItuNðPaB ΔT = +83.3o C . GnuvtþsmIkar 14-25 eTAelIGgát;elx @ Edl λ x = 0.707, λ y = 0.707 eyIg)an ⎡ (Q1 )0 ⎤ ⎡ 0.707 ⎤ ⎡ 0.000689325 ⎤ 1 ⎢(Q ) ⎥ ⎢ 0.707 ⎥ ⎢ ⎥ ⎢ (Q3 )0 ⎥ ( ) ⎢ 2 0 ⎥ = AE (11.7 ) 10 −6 (83.3)⎢ ⎥ = AE ⎢ 0.000689325 ⎥ 2 ⎢− 0.707 ⎥ ⎢− 0.000689325⎥ 7 ⎢ ⎥ ⎢ ⎥ ⎢ ⎥ ⎣(Q4 )0 ⎦ ⎣− 0.707 ⎦ ⎣− 0.000689325⎦ 8 m:aRTIsPaBrwgRkajsRmab; truss enHRtUv)anbegáItenAkñúg]TahrN_ 14-2. ⎡ 0 ⎤ ⎡ 0.135 0.035 0 0 0 − 0.1 − 0.035 − 0.035⎤ ⎡ D1 ⎤ ⎡ 0.000689325 ⎤ 1 ⎢ 0 ⎥ ⎢ 0.035 ⎥ ⎢D ⎥ ⎢ 0.000689325 ⎥ 2 ⎢ ⎥ ⎢ 0.135 0 − 0.1 0 0 − 0.035 − 0.035⎥ ⎢ 2 ⎥ ⎢ ⎥ ⎢ 0 ⎥ ⎢ 0 0 0.135 − 0.035 0.035 − 0.035 − 0.1 0 ⎥ ⎢ D3 ⎥ ⎢ 0 ⎥3 ⎢ ⎥ ⎢ ⎥⎢ ⎥ ⎢ ⎥ ⎢ 0 ⎥ = AE ⎢ 0 − 0.1 − 0.035 0.135 − 0.035 0.035 0 ⎥ ⎢ D4 ⎥ + AE ⎢ ⎥4 0 0 ⎢ 0 ⎥ ⎢ 0 0 0.035 − 0.035 0.135 − 0.035 0 − 0.1 ⎥ ⎢ D5 ⎥ ⎢ 0 ⎥5 ⎢ ⎥ ⎢ ⎥⎢ ⎥ ⎢ ⎥ ⎢Q 6 ⎥ ⎢ − 0.1 0 − 0.035 0.035 − 0.035 0.135 0 0 ⎥⎢ 0 ⎥ ⎢ 0 ⎥6 ⎢Q ⎥ ⎢− 0.035 − 0.035 − 0.1 0 0 0 0.135 0.035 ⎥⎢ 0 ⎥ ⎢− 0.000689325⎥ 7 ⎢ 7⎥ ⎢ ⎥⎢ ⎥ ⎢ ⎥ ⎣Q8 ⎥ ⎢ ⎦ ⎢− 0.035 ⎣ − 0.035 0 0 − 0.1 0 0.035 0.135 ⎥ ⎢ 0 ⎥ ⎦⎣ ⎦ ⎢− 0.000689325⎥ 8 ⎣ ⎦ edayBnøatedIm,IkMNt;smIkarbMlas;TIEdlCaGBaØat nigedayedaHRsayRbB½n§smIkarenH eyIg)an D1 = −0.002027m D2 = −0.01187 m Truss analysis using the stiffness method T.Chhay -495
  • 33. Department of Civil Engineering NPIC D3 = −0.002027m D4 = −0.009848m D5 = −0.002027m edayeRbIsmIkar 14-30 edIm,IkMNt;kmøaMgenAkñúgGgát;elx @ eyIg)an ⎡− 0.002027⎤ ⎢ − 0.01187 ⎥ 484[200] q2 = 10 2 [− 0.707 − 0.707 0.707 0.707]⎢ ⎢ 0 ⎥ − 484(200)11.7 10 −6 (83.3) ⎥ [ ( )] ⎢ ⎥ ⎣ 0 ⎦ = −27.09kN cMNaMfa kMeNInsItuNðPaBénGgát;elx @ nwgmineFVIeGaymankmøaMgRbtikmμenAelI truss eT edaysarva Ca truss kMNt;edaysþaTic. edIm,IbgðajBIkarBicarNakarBnøatm:aRTIsénsmIkar (1) edIm,IkMNt;kmøaMg Rbtikmμ. edayeRbIlT§plsRmab;bMlas;TI eyIg)an Q6 = AE[− 0.1(− 0.002027 ) + 0 − 0.035(− 0.002027 ) + 0.035(− 0.009828) − 0.035(− 0.002027 )] + AE [0] = 0 Q7 = AE[− 0.035(− 0.002027 ) − 0.035(− 0.01187 ) − 0.1(− 0.002027 ) + 0 + 0] + AE [− 0.000689325] = 0 Q8 = AE[− 0.035(− 0.002027 ) − 0.035(− 0.01187 ) + 0 + 0 − 0.1(− 0.002027 )] + AE [− 0.000689325] = 0 !$>(> karviPaK truss kñúglMh (Space-truss analysis) eKGacviPaK truss kñúglMhkMNt;edaysþaTic nig truss kñúglMhminkMNt;edaysþaTicedayeRbI dMeNIrkarviPaKdUcKñaEdl)anerobrab;BIelIkmun. b:uEnþ edIm,IKitG½kSTaMgbI eKRtUvbBa©ÚlFatubEnßmeTAkñúg m:aRTIsbMElg T . edIm,ITTYl)anva eyIgnwgBicarNaGgát; truss EdlbgðajenAkñúgrUbTI 14-17. m:aRTIsPaBrwgRkajsRmab;Ggát;EdlkMNt;edayeRbIkUGredaentMbn; x' RtUv)aneGayedaysmIkar 14-4. elIsBIenH tamkarGegátrUbTI 14-17 eKGackMNt;kUsIunUsR)ab;TiscenøaHkUGredaenskl nigkUGr- edaentMbn;edayeRbIsmIkarRsedogKñanwgsmIkar 14-5 nig 14-6 Edl xF − xN xF − xN λ x = cos θ x = = (14-31) L (x F − x N )2 + ( y F − y N )2 + ( z F − z N )2 yF − yN yF − yN λ y = cos θ y = = (14-32) L (x F − x N ) + ( y F − y N ) + (z F − z N ) 2 2 2 karviPaK truss edayeRbIviFIPaBrwgRkaj T.Chhay -496
  • 34. mhaviTüal½ysMNg;sIuvil viTüasßanCatiBhubec©keTskm<úCa zF − zN zF − zN λ z = cos θ z = = (14-33) L (x F − x N )2 + ( y F − y N )2 + ( z F − z N )2 CalT§plénTMhM ¬G½kS¦TIbI m:aRTIsbMElg ¬smIkar 14-9¦ køayCa ⎡λ x λ y λ z 0 0 0 ⎤ T =⎢ ⎥ ⎣ 0 0 0 λx λ y λz ⎦ edayCMnYsm:aRTIsenH nigsmIkar 14-4 eTAkñúgsmIkar 14-15 ¬ K = T T k 'T ¦ eyIg)an ⎡λ x 0⎤ ⎢λ 0⎥ ⎢ y ⎥ ⎢λ 0 ⎥ AE ⎡ 1 − 1⎤ ⎡λ x λ y λ z 0 0 0 ⎤ k=⎢ z ⎥ ⎢ ⎥ ⎢0 λ x ⎥ L ⎢− 1 1 ⎥ ⎣ 0 0 0 λ x λ y λ z ⎦ ⎣ ⎦ ⎢0 λy ⎥ ⎢ ⎥ ⎢0 ⎣ λz ⎥⎦ edayedaHRsayplKuNm:aRTIs eyIgnwgTTYl)anm:aRTIssIuemRTI Nx Ny Nz Fx Fy Fz ⎡ λ2 x λxλ y λxλz − λ2 x − λxλ y − λxλz ⎤ N x ⎢ ⎥ ⎢ λ y λx λ2 y λ y λ z − λ y λ x − λ2 − λ y λ z ⎥ N y y AE ⎢ k= λz λx λz λ y λ z − λ z λ x − λ z λ y − λ2 ⎥ N z 2 (14-34) L ⎢ z ⎥ ⎢ − λ2 x − λxλ y − λxλz λx2 λ x λ y λ x λ z ⎥ Fx ⎢ ⎥ ⎢− λ y λ x − λ2 y − λ y λz λ y λx λ2 y λ y λ z ⎥ Fy ⎢− λ λ − λz λ y − λ2 λ z λ x λ z λ y λ2 ⎥ Fz ⎣ z x z z ⎦ smIkarenHCam:aRTIsPaBrwgRkajsRmab;Ggát;Edl sresredayeRbIkUGredaenskl. elxkUdtam beNþayCYredk nigCYrQrtMNageGayTis x, y, z enARtg;cugCit N x , N y , N z Edlbnþedaycugq¶ay Fx , F y , Fz . sRmab;karsresrkmμviFIkMuBüÚT½r CaTUeTAvaman lkçN³gayRsYlkñúgkareRbIsmIkar 14-34 Cagkar edaHRsayplKuNm:aRTIs T T k 'T sRmab;Ggát; nImYy². dUckarerobrab;BIxagedIm dMbUgkMuBüÚT½rnwg rkSam:aRTIsPaBrwgRkajsRmab;rcnasm½<n§ K Edl manFatuesμIsUnü bnÞab;mkeTotedaysarFatunImYy² énm:aRTIsPaBrwgRkajsRmab;Ggát;RtUv)anbegáIt vaRtUv)andak;eTAkñúgTItaMgRtUvKñarbs;vaenAkñúgm:aRTIs K . eRkayeBlFaturbs;m:aRTIsPaBrwgRkaj Truss analysis using the stiffness method T.Chhay -497
  • 35. Department of Civil Engineering NPIC sRmab;rcnasm<½n§RtUv)anbegáIt eKGacGnuvtþdMeNIrkar Edl)anerobrab;enAkñúgkfaxNÐ 14-6 edIm,I kMNt;bMlas;TIrbs;tMN kmøaMgRbtikmμ nigkmøaMgkñúgrbs; Ggát;. karviPaK truss edayeRbIviFIPaBrwgRkaj T.Chhay -498
  • 36. mhaviTüal½ysMNg;sIuvil viTüasßanCatiBhubec©keTskm<úCa cMeNaT 14>1 kMNt;m:aRTIsPaBrwgRkaj K sRmab;eRKOg 14>6 kMNt;m:aRTIsPaBrwgRkaj K sRmab; truss. bgÁúM. yk A = 300mm 2 nig E = 200GPa yk A = 0.005m 2 nig E = 200GPa . snμt; sRmab;Ggát;. tMNTaMgGs;tP¢ab;edaysnøak;. 14>2 kMNt;bMlas;TItamTisedk nigTisQr enARtg;tMN ③ rbs;eRKOgbgÁúMenAkñúgcMeNaT 14>1. 14>7 kMNt;bMlas;TItamTisQrenARtg;tMN ① 14>3 kMNt;kmøaMgkñúgénGgát;nImYy²rbs;eRKOg nigkmøaMgkñúgrbs;Ggát;elx @ éncMeNaT 14>6. bgÁúMenAkñúgcMeNaT 14>1. 14>8 kMNt;m:aRTIsPaBrwgRkaj K sRmab; truss. 14>4 kMNt;m:aRTIsPaBrwgRkaj K sRmab; truss. yk A = 0.0015m 2 nig E = 200GPa sRmab; yk A = 300mm 2 nig E = 200GPa sRmab; Ggát;. Ggát;. 14>5 kMNt;bMlas;TItamTisQrenARtg;tMN ④ nigkmøaMgkñúgrbs;Ggát;elx $ éncMeNaT 14>4. 14>9 kMNt;kmøaMgkñúgénGgát;elx ^ éncMeNaT yk A = 0.0015m 2 nig E = 200GPa . 14>8. yk A = 0.0015m 2 nig E = 200GPa Problems T.Chhay -499
  • 37. Department of Civil Engineering NPIC sRmab;Ggát;nImYy². 14>13. yk A = 1000mm 2 nig E = 14>10 kMNt;kmøaMgkñúgénGgát;elx ! éncMeNaT 200GPa . 14>8 RbsinebI Ggát;EvgCagmun10mm munnwg 14>15 kMNt;kmøaMgkñúgénGgát;elx @éncMeNaT P¢ab;vaeTAkñúg truss. edIm,IedaHRsay dkbnÞúk 14>8 RbsinebIsItuNðPaBekIneLIg 55o C . 10kN ecj. yk A = 0.0015m 2 nig E = yk A = 1000mm 2 E = 200GPa nig α = 200GPa sRmab;Ggát;nImYy². 11.7(10 −6 )/ o C . 14>11 kMNt;m:aRTIsPaBrwgRkaj K sRmab; 14>16 kMNt;kmøaMgRbtikmμenAelI truss. AE truss. AE CacMnYnefr. CacMnYnefr. 14>12 kMNt;kmøaMgkñúgénGgát;elx @ nig elx % éncMeNaT 14>11. AE CacMnYnefr. 14>13 kMNt;m:aRTIsPaBrwgRkaj K sRmab; truss. yk A = 1000mm 2 nig E = 200GPa . 14>14 kMNt;bMlas;TItamTisedkenARtg;tMN ① nigkmøaMgkñúgrbs;Ggát;elx @ éncMeNaT cMeNaT T.Chhay -500