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CPP 301 Core Project Part I



DESIGNING OF A NOISE BARRIER




                      Submitted by
      Lalit Aggarwal &Gayathri Lakshmi Kulukuru


                       Supervisor
                    Dr. Navin Kumar


   School of Mechanical Materials & Energy Engineering

INDIAN INSTITUTE OF TECHNOLOGY ROPAR
                        Nov 2012

                          ~1~
CERTIFICATE


This report is submitted by Mr.Lalit Aggarwal &Ms.Gayathri Lakshmi Kulukuru detailing
the work done during the 1st semester, 2011-2012. The report written and all material taken
from other sources(books, manuals, journals,etc.) have been fully acknowledged.




Lalit Aggarwal                                        Gayathri Lakshmi Kulukuru
P2009ME1085                                           P2009ME1062
SMMEE, IIT Ropar                                      SMMEE, IIT Ropar
Date: 09-Nov-2012                                     Date: 09-Nov-2012




Mr. Lalit Aggarwal &Ms.Gayathri Lakshmi Kulukuru have worked under my supervision
during this semester. I have read this report; it meets the expectations and it accurately
reflects the work done by the students.




Dr. Navin Kumar
(Supervisor)
Date: 08-Nov-2012




                                             ~2~
ACKNOWLEDGMENTS

The authors acknowledge the support of the Director, Defense and Research Organization
(DRDO) for giving the opportunity to work on the project. The authors acknowledge the
guidance acquired from the project work of Mr. SahilBagat performed in the previous year.
The authors acknowledge the support of their Project advisor Dr. Naveen Kumar for their
continuous guidance and support throughout the semester.




Lalit Aggarwal                                     Gayathri Lakshmi Kulukuru
P2009ME1085                                        P2009ME1062
SMMEE, IIT Ropar                                   SMMEE, IIT Ropar




                                          ~3~
ABSTRACT


The project which was given to us addressed the investigation of the technical, aesthetic, and
economic feasibility of deploying special noise barrier application into baffle range of
DRDO.

So we have to suggest a most suitable design of noise and maximum sound attenuation can be
achieved under having some constraints like cost, weight and aesthetic requirements.


Sound attenuation in noise barrier depends on various parameters like (height, type of
material, top surface modification, receiver or source position and several other parameters,
barrier shapes).
There is a threefold process in which we are going to do this project.

1. Literature Survey and Theory.
2. Modeling and calculating Results.
3. Make prototypes and Verifying Results.

In Literature Survey in which there a cumulative study about the past design, all the research
done in the field and all of the different possibility is there in designing. In order to
understand the physics behind it thorough study about the theory of acoustics design is also
required.

In Modeling, Using Sysnoise software the problem will be modeled and result will be
obtained and compared with the theoretical results. Simple barrier can be solved analytically
using empirical relations but advanced barrier needs BEM or Some kind of simulation
software (SYSNOISE). The simulation will help in estimating the behavior of the noise
barrier under different parameters e.g.- changes in the barrier parameter, change in material
and other parameters.

In making Prototype and verifying results, there is series of experiments have to be
performed to see the practical behavior of the parameters involved in the formulation of the
problem which is performed using microphone and other devices.

Then all the results will be analyzed and final design will be made.

In this report we continued our work after internship work from literature survey to modeling
in matlab and taking physical readings from existing wall and on wooden barrier. Then we
compared this reading with problem formulated in Matlab and with software output. Software
we used was Oliver Lab Terrain.




                                            ~4~
TABLE OF CONTENTS
ABSTRACT ........................................................................................................................... 4
Problem statement and motivation ........................................................................................ 7
INTRODUCTION .................................................................................................................. 7
REVIEW OF PAST WORK.................................................................................................... 8
      Conclusion from literature ............................................................................................ 12
Work done in this semester ................................................................................................. 13
   Experiment work .............................................................................................................. 13
   MATLAB Programming .................................................................................................... 15
   MODELLING IN OLIVE LAB TERRAIN ........................................................................... 18
   Comparison of results with experimental results .............................................................. 22
Future Work ........................................................................................................................ 23
   References ...................................................................................................................... 23




                                                              ~5~
LIST OF TABLES & FIGURES
Table 1 Literature related to insertion losses in a barrier sorted based on the parameters
being varied .......................................................................................................................... 9
Figure 1 Noise barriers with various shape edges and surface conditions............................. 8
Figure 2 Schematic of the experiment performed ................................................................ 13
Figure 3 Experimental Setup for the soft ground ................................................................ 13
Figure 4 Experiment setup for hard ground ......................................................................... 14
Figure 5Definitions of symbols used to determine Fresnel Number ‘N’ ................................ 15
Figure 6Paths considered in Lam Method ........................................................................... 16
Figure 7 Flowchart of the matlab code ................................................................................ 16
Figure 8 Matlab GUI ............................................................................................................ 17
Figure 9 Comparison of insertion losses with change in height at different frequencies ...... 18
Figure 10Comparison of insertion losses with frequency variation at different heights ........ 19
Figure 11 Variation of thickness .......................................................................................... 20
Figure 12 a) single panel barrier                             b) double panel barrier ......................................... 20
Figure 13 IL variation in single and double panels (frequency=1000hz) .............................. 21
Figure 14 IL variation in single and double panels (frequency=2000hz) .............................. 21
Figure 15Comparision of matlab and software results with experimental results at 500 Hertz
........................................................................................................................................... 22
Figure 16Comparisonof MATLAB and software results with Experimental results at 1000
Hertz ................................................................................................................................... 22




                                                                  ~6~
PROBLEM STATEMENT AND MOTIVATION

Specific Aim: To design an effective and cost-efficient noise barrier for the baffle range
which can reduce the unwanted noise up to the required level.

Usually firing ranges where soldiers are trained for the shooting at different conditions are
made out of the city so that there was no disturbance to the local residents. But some of the ranges are
within the residential areas where common people feel a lot of noise. So, to get the control over this
type of noise a noise barrier need to be designed around the range to reduce the noise up to a desirable
level.


                                    INTRODUCTION
Increasing noise pollution will lead to an ever increasing need to control noise of all forms.
Noise barriers are the most common solution for controlling noise from surroundings and
several methods have been developed for improving their efficiency without increasing their
height.
Examples of already deployed noise barriers in India:
1.       Noise Barriers in BKC, Mumbai (2010)
2.       IIT Powai noise barrier (2012)
3.       Commonwealth Games noise barrier (2010)
4.       Sound barriers at Suman Nagar, Navghar flyovers (2012)
The vast majority of these have been vertical, reflective wall made of concrete, wood or steel.
The standard top for these walls is a “knife-edge”, providing a single diffraction edge with a
reflective diffraction zone.
Clearly, there are many other options for noise barrier shapes than vertical reflective walls
with knife-edge diffraction zone. In addition to it, there are option to make barriers
absorptive, to displace the diffraction zone through the use of a slanted section on top, or to
provide for a double- diffraction zone through the use of a T-top section and other modified
tops of the walls.




                                                ~7~
REVIEW OF PAST WORK
During summer internship most of the literature work was performed and all the work is
presented in the tabular form in table 1 and table 2. During this time also complete study was
performed and the entire phenomenon was studied.

Different types of barrier that were studied are:

           -   Shaped Barrier
           -   Conventional Barrier
           -   T-shaped barrier
           -   Multiple Edge Barrier
           -   Arrow shape Barrier


Figure 1 illustrates various noise barriers obtained by varying the shape edges and surface
conditions.




   FIGURE 1: NOISE BARRIERS W ITH VARIOUS SHAPE EDGES AND SURFACE CONDITIONS




                                             ~8~
TABLE 1LITERATURE RELATED TO INSERTION LOSSES IN A BARRIER SORTED BASED ON
                                         THE PARAMETERS BEING VARIED

Different
barrier            Simple        T-top             y-top      Cylindrical   Wedge      Multipl    Angled edge
Parameter                                                    top            shaped     e edge

Barrier height     D. C.         David J.
                   HOTHERSA      Oldham ,
                   LL, S. N.     Christopher A.
                   CHANDLER      Egan (2011)
                   -WILDE
                   AND M. N.     P.J. Thorsson
                   HAJMIRZAE     (2003)
                   (1990)

                   Takashi
                   Ishizuka*,
                   Kyoji
                   Fujiwara
                   (2003)
Change in                        David J.                                                         D J Oldham and C A Egan
source position                  Oldham ,                                                         (2009)
                                 Christopher A.
                                 Egan (2011)


                   D. C.         D. C.                                      D. C.
                   HOTHERSA      HOTHERSALL                                 HOTHER
Receiver height    LL, S. N.     , S. N.                                    SALL, S.
                   CHANDLER      CHANDLER-                                  N.
                   -WILDE        WILDE AND                                  CHANDL
                   AND M. N.     M. N.                                      ER-
                   HAJMIRZAE     HAJMIRZAE(1                                WILDE
                   (1990)        990)                                       AND M.
                                                                            N.
                                                                            HAJMIR
                                                                            ZAE(1990
                                                                            )
Change in          A. Muradali   David J.                                   D. C.      C.A.
receiver           and K. R.     Oldham ,                                   HOTHER     Egan, V
position           Fyfe (1994)   Christopher A.                             SALL, S.   Chilekw
                                 Egan (2011)                                N.         a and D.
                   D. C.         D. C.                                      CHANDL     J.
                   HOTHERSA      Hothersall, D.                             ER-        Oldham
                   LL, S. N.     H. Crombie &                               WILDE      (2006)
                   CHANDLER      S. N. Chandler-                            AND M.
                   -WILDE        Wilde                                      N.
                   AND M. N.                                                HAJMIR
                   HAJMIRZAE     C.A. Egan, V                               ZAE(1990
                   (1990)        Chilekwa and                               )
                                 D. J.
                                 Oldham(2006)

                                 D. C.
                                 HOTHERSALL
                                 , S. N.
                                 CHANDLER-
                                 WILDE AND
                                 M. N.


                                                           ~9~
HAJMIRZAE(1
                               990)




Width of top                   David J.                                                    D. H.
                               Oldham ,                                                    Crombi
                               Christopher A.                                              e, D. C.
                               Egan (2011)                                                 Hothers
                                                                                           all& S.
                               D. C.                                                       N.
                               Hothersall, D.                                              Chandle
                               H. Crombie &                                                r-Wilde
                               S. N. Chandler-                                             (1994)
                               Wilde                                                       C.A.
                                                                                           Egan, V
                               C.A. Egan, V                                                Chilekw
                               Chilekwa and                                                a and D.
                               D. J.                                                       J.
                               Oldham(2006)                                                Oldham
                                                                                           (2006)
Cap depth                      D. C.                               TomonaoO                D. H.
                               Hothersall, D.                      kuboa) and              Crombi
                               H. Crombie &                        Kyoji                   e, D. C.
                               S. N. Chandler-                     Fujiwara                Hothers
                               Wilde                                                       all& S.
                               P.J. Thorsson                                               N.
                               (2003)                                                      Chandle
                                                                                           r-Wilde
                                                                                           (1994)
                                                                                D. C.                 D J Oldham and C A Egan
Angle variation                                                                 HOTHER                (2009)
                                                                                SALL, S.
                                                                                N.
                                                                                CHANDL
                                                                                ER-
                                                                                WILDE
                                                                                AND M.
                                                                                N.
                                                                                HAJMIR
                                                                                ZAE(1990
                                                                                )
                                                 D. C.
                  Takashi                        Hothersall, D.    Takashi      D. C.      Takashi    Takashi Ishizuka*, Kyoji
Comparison        Ishizuka*,                     H. Crombie &      Ishizuka*,   HOTHER     Ishizuka   Fujiwara (2003)
with T-top        Kyoji                          S. N. Chandler-   Kyoji        SALL, S.   *, Kyoji
                  Fujiwara                       Wilde(1990)       Fujiwara     N.         Fujiwar
                  (2003)                                           (2003)       CHANDL     a (2003)
                                                 Takashi                        ER-
                  D. C.                          Ishizuka*,                     WILDE
                  HOTHERSA                       Kyoji Fujiwara                 AND M.
                  LL, S. N.                      (2003)                         N.
                  CHANDLER                                                      HAJMIR
                  -WILDE                                                        ZAE
                  AND M. N.                                                     (1990)
                  HAJMIRZA
                  E (1990)



                                                           ~ 10 ~
barrier surface   David J.       David J.                                         D. C.      D. H.      D J Oldham and C A Egan
variation         Oldham ,       Oldham ,                                         HOTHER     Crombi     (2009)
                  Christopher    Christopher A.                                   SALL, S.   e, D. C.
                  A. Egan        Egan (2011)                                      N.         Hothers
                  (2011)                                                          CHANDL     all& S.
                  D. C.          P.J. Thorsson                                    ER-        N.
                  HOTHERSA       (2003)                                           WILDE      Chandle
                  LL, S. N.                                                       AND M.     r-
                  CHANDLER                                                        N.         Wilde(1
                  -WILDE                                                          HAJMIR     994)
                  AND M. N.                                                       ZAE(1990
                  HAJMIRZA                                                        )
                  E(1990)
 top surface                     David J.          D. C.                                     D. H.      D J Oldham and C A Egan
absorption                       Oldham ,          Hothersall, D.                            Crombi     (2009)
variation                        Christopher A.    H. Crombie &      Takashi                 e, D. C.
                                 Egan (2011)       S. N. Chandler-   Ishizuka*,              Hothers
                                                   Wilde (1990)      Kyoji                   all& S.
                                 D. C.                               Fujiwara                N.
                                 Hothersall, D.                      (2003)                  Chandle
                                 H. Crombie &                                                r-
                                 S. N. Chandler-                                             Wilde(1
                                 Wilde                                                       994)

                                 C.A. Egan, V                                                C.A.
                                 Chilekwa and                                                Egan, V
                                 D. J.                                                       Chilekw
                                 Oldham(2006)                                                a and D.
                                                                                             J.
                                 D. C.                                                       Oldham
                                 HOTHERSALL                                                  (2006)
                                 , S. N.
                                 CHANDLER-
                                 WILDE AND
                                 M. N.
                                 HAJMIRZAE(1
                                 990)

                                 M.R.
                                 Monazzam,
                                 Y.W.
                                 Lam(2006)
Ground surface    Muradali and   D. C.
variation         K. R. Fyfe     Hothersall, D.
                  (1994)         H. Crombie &
                                 S. N. Chandler-
                  D. C.          Wilde
                  HOTHERSA
                  LL, S. N.      P.J. Thorsson
                  CHANDLER       (2003)
                  -WILDE
                  AND M. N.
                  HAJMIRZA
                  E(1990)




                                                             ~ 11 ~
MahdiyehNader
Perforated                     zadeh a,⇑,
sheet on                       Mohammad
diffuser                       Reza Monazzam
                               b, ParvinNassiri
                               b,
                               SamanehMome
                               nBellahFard
                               (2011)
QRD on top                     M.R.
                               Monazzam,
                               Y.W.
                               Lam(2006)
                               MahdiyehNader
                               zadeh a,⇑,
                               Mohammad
                               Reza Monazzam
                               b, ParvinNassiri
                               b,
                               SamanehMome
                               nBellahFard(20
                               11)
Soft                                                            TomonaoO
                                                                kuboa) and
                                                                Kyoji
                                                                Fujiwara



Reflective top                                                                          D. H.      D J Oldham and C A
                                                                                        Crombi     Egan(2009)
                                                                                        e, D. C.
                                                                                        Hothers
                                                                                        all& S.
                                                                                        N.
                                                                                        Chandle
                                                                                        r-
                                                                                        Wilde(1
                                                                                        994)



                                        CONCLUSION FROM LITERATURE


             Going through all the research papers and by seeing their comparative study, it was vaguely
             suggested that T-type barrier having absorptive coating suits best to get maximum sound
             abatement.

             Since for a single barrier height/cost ration peaks at 3meter so height of T-top barrier should
             be taken 3meter and width of the top can be taken as 1 meter so that aesthetically is looks
             good and having maximum sound abatement.

             Till internship the project was not having any practical touch and in this research paper
             experiments were conducted and results was compared to get the real and practical touch




                                                         ~ 12 ~
WORK DONE IN THIS SEMESTER

                             EXPERIMENT WORK

                                     SCHEMATIC




                 FIGURE 2: SCHEMATIC OF THE EXPERIMENT PERFORMED




Figure 2 shows the basic schematics of the experiments that were performed and it shows
various parameter that is involved during calculations.



           EXPERIMENT ON SOFT GROUND FOR AN EXISTING WALL




                FIGURE 3 : EXPERIMENTAL SETUP FOR THE SOFT GROUND


                                        ~ 13 ~
Figure 3 shows the experiment that was performed on an existing wall at the fuel-zap in IIT
Ropar to get the basic insight of the insertion loss values obtained. The material of the wall is
concrete with a height of 170 cm and thickness of 22 cm. The parameters that are varied in
this experiment are frequency (varied between 100-1000Hz at an interval of 100 Hz) and
receiver distance (varied between 3-15m from the wall) while keeping all other parameters
constant. The source height and receiver height are kept in the shadow region with values of
50 cm and 100 cm respectively.

                            EXPERIMENT ON HARD GROUND




                      FIGURE 4EXPERIMENT SETUP FOR HARD GROUND

The experiment was performed on a finite barrier on hard ground to enable comparisons as
most of the analytical solutions are for hard ground. Figure 4 shows the experimental setup of
the experiment. The material of the barrier is wood with a height of 90 cm, width of 108 cm
and thickness of 2 cm. The parameters that are varied in this experiment are frequency
(varied between 100-1000Hz at an interval of 100 Hz) and receiver distance (varied between
0-16m from the barrier) while keeping all other parameters constant. The source height and
receiver height are kept in the shadow region with values of 50 cm and 83 cm respectively.




                                            ~ 14 ~
MATLAB PROGRAMMING
            THEORY: LAM’S METHOD USING MAEKAWA’S CURVE

Maekawa introduced an empirically based diffraction model that provides the insertion loss
due to a thin-walled barrier in terms of the Fresnel number.Maekawa then suggested that the
insertion loss for a finite-length barrier could be determined by multiple application of this
curve to the diffraction paths around the barrier and then summing the energy contributions
of these paths.


       Maekawa‟s curve can be represented by the following two equations:




       where N is Fresnel Number given by



Where (A+B-d) is the path difference and λ is the wavelength. The symbols are defined as
shown in the Figure 5.




 FIGURE 5 DEFINITIONS OF SYMBOLS USED TO DETERMINE FRESNEL NUMBER ‘N’




Lam improved on Maekawa‟s method by summing complex pressures, instead of energies, of
each diffraction path around the barrier. This was done to incorporate the phase interaction
and interference between the paths, the absence of which, Lam suggested, was the cause of
the poor agreement between Maekawa‟s method and experimental results.
A semi-infinite barrier is equivalent to a 2D geometry. Diffraction Paths considered for a
semi-infinite thin barrier are as shown in Figure 6.
                                           ~ 15 ~
FIGURE 6 PATHS CONSIDERED IN LAM METHOD

       The barrier insertion loss is given by:




Mi represents the insertion loss value from Maekawa‟s curve for the ithpath. The subscript „o‟
refers to the direct path (from the source to receiver) and the subscript „r‟ refers to the ground
reflected path (from the source image to receiver).

The Lam method fell short when the receivers were in the proximity of the line-of-sight, and
when parallel geometries in 2D were considered. This is due to the fact that this method does
not predict a unique phase shift at the diffraction edge for each path.



                                  GUI IMPLEMENTATION




                        FIGURE 7: FLOWCHART OF THE MATLAB CODE


                                             ~ 16 ~
A MATLAB GUI has been made for calculating the insertion loss. It includes analysis for an
input data.

A GUI (graphical user interface) allows users to perform tasks interactively through controls
such as buttons and sliders. Within MATLAB®, GUI tools enable you to perform tasks such
as creating and customizing plots, fitting curves and surfaces, and analyzing and filtering
signals.

Figure 8 shows the typical GUI that was modeled in the Matlab using Lam‟s equation.
Parameters that were involved in GUI are barrier height, Source and receiver height, source
and receiver distance, and frequency of the sound.

It also shows the graphical variation of the variation in one parameter by taking 5 other
parameter constant and vary 6th one.




                                    FIGURE 8 MATLAB GUI




                                           ~ 17 ~
MODELLING IN OLIVE LAB TERRAIN
                                                     ABOUT THE SOFTWARE
THEORY
The acoustic calculations are made by the software based on Hadden& Pierce Diffraction 3D
model implemented with finite impedances faces using Salomons semi-analytical method
including ground effects. Multiple barrier diffraction is calculated in a recursive way at any
diffraction order.Ground effect is included using the One Parameter Theory of Chessell based
on Delany and Bazley.
LIMITATIONS
The thickness of the barrier cannot be reduced to a value less than 3cm. The numerical values
of the readings are available only at octave and 1/3rd octave frequencies. Any other parameter
except frequency cannot be varied in the same model.

                                                        ANALYSIS MADE
                                                      VARIATION OF HEIGHT


                                                                                PARAMETERS
                                                                                Barrier Material: mineral wool

                                                                                Barrier type: Thin Barrier

                                                                                Receiver Height= 50 cm

                                                                                Source Height= 50cm

                                                                                Source distance=5m



                                   35

                                   30
           Insertion Loss(in dB)




                                   25

                                   20
                                                                                               1000 Hz
                                   15
                                                                                               1995 Hz
                                   10
                                                                                               3981 Hz
                                    5

                                    0
                                        0        1         2             3      4          5
                                                         Barrier height(in m)

  FIGURE 9: COMPARISON OF INSERTION LOSSES WITH CHANGE IN HEIGHT AT DIFFERENT
                                  FREQUENCIES



                                                             ~ 18 ~
35

                               30

                               25
       Insertion Loss(in dB)




                               20                                                          h=1m
                                                                                           h=2m
                               15
                                                                                           h=3m
                               10                                                          h=4m

                                5

                                0
                                    2   2.5            3              3.5              4
                               -5
                                              log(frequency(in Hz))

     FIGURE 10: COMPARISON OF INSERTION LOSSES WITH FREQUENCY VARIATION AT
                                DIFFERENT HEIGHTS

It can be seen that the insertion loss increases with increase of barrier height. From the figure
7, it can be seen that the variation of the insertion loss values is not much when it is changed
from a height of 3m to 4m.



                                         VARIATION OF THICKNESS
MASS LAW
When sound is incident upon a wall or partition, some of it will be reflected and some will be
transmitted through the wall. The transmission loss obtained can be determined using mass
law at a particular frequency.



Where m=mass density and

          f=frequency
                                                                      PARAMETERS
                                                                      Barrier Material: mineral wool

                                                                      Flow resistivity=20000 Pas/m2

                                                                      Barrier Height = 2m

                                                                      Receiver Height= 1 m

                                                                      Source Height = 1 m

                                                                      Source distance=2m



                                                   ~ 19 ~
Frequency=1500 Hz



                                30

                                25

                                20
        Insertion Loss(in dB)




                                                                                     thickness_3cm
                                15
                                                                                     thickness_3.5cm
                                                                                     thickness_4cm
                                10                                                   thickness_4.5cm

                                 5

                                 0
                                     0   10        20         30           40   50            60
                                -5
                                                    Receiver distance (in m)

                                          FIGURE 11 VARIATION OF THICKNESS

From figure 8 it can be clearly seen that the value of insertion loss doesn‟t vary much with
the receiver distance for thickness values greater than the optimum value calculated from the
mass law (≈2.5cm).

                                              SINGLE VS DOUBLE PANELS




FIGURE 12 A) SINGLE PANEL BARRIER                           B) DOUBLE PANEL BARRIER

PARAMETERS
Barrier Material: mineral wool
Flow resistivity        20000 Pas/m2
Barrier Height          2m
Barrier Thickness       20cm single
                        10 cm double
Receiver Height         1m
Source Height           1m
Source distance         2m




                                                        ~ 20 ~
45
                                                                                      Frequency = 1000 Hz
                           40

                           35
                                                                                           single panel
                           30

                           25
                                                                                           double
   Insertion Loss(in dB)




                           20                                                              panel_gap20cm

                           15                                                              double panel_gap
                                                                                           30cm
                           10

                            5                                                              double
                                                                                           panel_gap50cm
                            0
                                0    2       4          6          8        10        12
                                             Receiver distance(in m)


                           FIGURE 13 IL VARIATION IN SINGLE AND DOUBLE PANELS (FREQUENCY=1000HZ)




                           45

                           40

                           35                                                         Frequency = 2000 Hz
   Insertion Loss(in dB)




                           30
                                                                                           single panel
                           25
                                                                                           double panel gap
                           20                                                              20 cm
                                                                                           double panel_gap
                           15
                                                                                           30cm
                           10                                                              double
                                                                                           panel_gap50cm
                            5

                            0
                                0    2       4         6         8     10        12
                                            Receiver distance (in m)



                           FIGURE 14 IL VARIATION IN SINGLE AND DOUBLE PANELS (FREQUENCY=2000HZ)

From the figures 13 and 14 it can be clearly seen that double panel barriers are more effective
in sound reduction compared to single panel barrier and the insertion loss increases with
increase in gap between the two panels.




                                                             ~ 21 ~
COMPARISON OF RESULTS WITH EXPERIMENTAL RESULTS

PARAMETERS
Barrier Material: wood
Barrier Height=90 cm
Barrier Width=105 cm
Barrier Thickness= 2cm
Receiver Height= 80 cm
Source Height= 50 cm




   FIGURE 15 COMPARISION OF MATLAB AND SOFTWARE RESULTS WITH EXPERIMENTAL
                             RESULTS AT 500 HERTZ




    FIGURE 16COMPARISONOF MATLAB AND SOFTWARE RESULTSWITH EXPERIMENTAL
                           RESULTSAT 1000 HERTZ

From the figures 15 and 16 it can be seen that the results from the software are in coherence
with those of the experimental results within acceptable error limits. It can also be seen there
is a considerable variation in the results obtained from MATLAB program, the reasons of
which can be attributed to the assumptions made in the theoretical model, where it considers
the barrier is semi-infinite with negligible thickness and which doesn‟t include the effect of
the material of the barrier.


                                            ~ 22 ~
FUTURE WORK

Some part of the project is completed in B.Tech-1 project which was in this semester and this
project will be continued in coming semester also as B.Tech-2 project.

The things which are planned for coming semester are:

   1. In current work, Material selection for the barrier was not suggested so work will be
      done in this context in the upcoming semester.

   2. In current work, output from the software of single and double panels was compared
      but there physical modelling was not done. It will be includedin the further studies.

   3. The software which is presently used has certain limitations due to which one cannot
      vary the shape of the barrier. The new software SYSNOISE, which is BEM/FEM
      software, was purchased for getting more accurate results and help in physical
      modelling of the system.

   4. In current study the MATLAB formulations are donefor a semi-infinite, thin barrier.
      In 2nd part the more focus will be made in including parameters like thickness,
      finiteness, etc.

   5. In our next work formation of the optimization problem will be included and will be
      solved using different optimization techniques.




                                  REFERENCES
        Web site reference

   1. http://sciencedirect.com/
   2. http://www.acoustax.com/noise-barrier-specs.php
   3. http://www.acousticalsurfaces.com/wall_barrier/wall_barrier.htm
   4. http://www.nrc-cnrc.gc.ca/eng/ibp/irc/bsi/85-sound-tranmission.html
   5. http://articles.timesofindia.indiatimes.com/2012-05-17/mumbai/31747986_1_noise-
      barrier-noise-levels-sumaira-abdulali
   6. http://www.nrc-cnrc.gc.ca/eng/ibp/irc/bsi/85-sound-tranmission.html
   7. http://www.otlterrain.com/



Research Papers

   [1] R.O.Feher, proc.Ann.Nat. Noise Abatement Symp.,1951,p-98
   [2] A.Muradali and K.R Fyfe,A study of 2d and 3d barrier insertion loss using
       improved diffraction based methods, applied acoustics,vol.53,no-1-3,pp 49-75,1998
   [3] D. C. HOTHERSALL, S. N. CHANDLER-WILDE AND M. N. HAJMIRZAE,
       Efficiency of Single Noise barrier, Journal of Sound and Vibration (1991) 146(2),
       303-322.


                                          ~ 23 ~
[4] David J. Oldham , Christopher A. Egan.. A parametric investigation of the
    performance of T-profiled highway noise barriers.. Applied Acoustics 72 (2011)
    803–813
[5] C.A. Egan, V Chilekwa and D. J. Oldham, Top edge treatment to enhance the
    performance of a noise,Acoustics Research Unit, University of LiverpoolLiverpool,
    L69 3BX, United Kingdom
[6] Watts, G.R., Barrier design to reduce road traffic noise. Proceedings of the
    Institution of Civil Engineers, 2002. 53(2): p. 79- 86.
[7] Takashi Ishizuka, KyojiFujiwara,Performance of noise barriers with various edge
    shapes and acoustical conditions.. Applied Acoustics 65 (2004) 125–141.
[8] MahdiyehNaderzadeh, Mohammad Reza Monazzam, ParvinNassiri,
    SamanehMomenBellahFard, Application of perforated sheets to improve the
    efficiency of reactive profilednoise barriers, Applied Acoustics 72 (2011) 393–398.
[9] A. Muradali and K. R. Fyfe, A Study of 2D and 3D Barrier Insertion Loss using
    Improved Diffraction-based Methods, Applied Acoustics, Vol. 53, No. I-3, pp. 49-
    15, 1998
[10]         Maekawa, Z., Noise reduction by screens. Applied Acoustics, 1968, 1, 157-
    173.
[11]         Pontus J. Thorsson,Combined effects of admittance optimisationon both
    barrier and ground, Applied Acoustics 64 (2003) 693–711.
[12]         D J Oldham and C A Egan, The development of a practical top edge device for
    a noise barrier, 16th international congress on noise and vibration July 2009.




                                      ~ 24 ~

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Btp report final_lalit

  • 1. CPP 301 Core Project Part I DESIGNING OF A NOISE BARRIER Submitted by Lalit Aggarwal &Gayathri Lakshmi Kulukuru Supervisor Dr. Navin Kumar School of Mechanical Materials & Energy Engineering INDIAN INSTITUTE OF TECHNOLOGY ROPAR Nov 2012 ~1~
  • 2. CERTIFICATE This report is submitted by Mr.Lalit Aggarwal &Ms.Gayathri Lakshmi Kulukuru detailing the work done during the 1st semester, 2011-2012. The report written and all material taken from other sources(books, manuals, journals,etc.) have been fully acknowledged. Lalit Aggarwal Gayathri Lakshmi Kulukuru P2009ME1085 P2009ME1062 SMMEE, IIT Ropar SMMEE, IIT Ropar Date: 09-Nov-2012 Date: 09-Nov-2012 Mr. Lalit Aggarwal &Ms.Gayathri Lakshmi Kulukuru have worked under my supervision during this semester. I have read this report; it meets the expectations and it accurately reflects the work done by the students. Dr. Navin Kumar (Supervisor) Date: 08-Nov-2012 ~2~
  • 3. ACKNOWLEDGMENTS The authors acknowledge the support of the Director, Defense and Research Organization (DRDO) for giving the opportunity to work on the project. The authors acknowledge the guidance acquired from the project work of Mr. SahilBagat performed in the previous year. The authors acknowledge the support of their Project advisor Dr. Naveen Kumar for their continuous guidance and support throughout the semester. Lalit Aggarwal Gayathri Lakshmi Kulukuru P2009ME1085 P2009ME1062 SMMEE, IIT Ropar SMMEE, IIT Ropar ~3~
  • 4. ABSTRACT The project which was given to us addressed the investigation of the technical, aesthetic, and economic feasibility of deploying special noise barrier application into baffle range of DRDO. So we have to suggest a most suitable design of noise and maximum sound attenuation can be achieved under having some constraints like cost, weight and aesthetic requirements. Sound attenuation in noise barrier depends on various parameters like (height, type of material, top surface modification, receiver or source position and several other parameters, barrier shapes). There is a threefold process in which we are going to do this project. 1. Literature Survey and Theory. 2. Modeling and calculating Results. 3. Make prototypes and Verifying Results. In Literature Survey in which there a cumulative study about the past design, all the research done in the field and all of the different possibility is there in designing. In order to understand the physics behind it thorough study about the theory of acoustics design is also required. In Modeling, Using Sysnoise software the problem will be modeled and result will be obtained and compared with the theoretical results. Simple barrier can be solved analytically using empirical relations but advanced barrier needs BEM or Some kind of simulation software (SYSNOISE). The simulation will help in estimating the behavior of the noise barrier under different parameters e.g.- changes in the barrier parameter, change in material and other parameters. In making Prototype and verifying results, there is series of experiments have to be performed to see the practical behavior of the parameters involved in the formulation of the problem which is performed using microphone and other devices. Then all the results will be analyzed and final design will be made. In this report we continued our work after internship work from literature survey to modeling in matlab and taking physical readings from existing wall and on wooden barrier. Then we compared this reading with problem formulated in Matlab and with software output. Software we used was Oliver Lab Terrain. ~4~
  • 5. TABLE OF CONTENTS ABSTRACT ........................................................................................................................... 4 Problem statement and motivation ........................................................................................ 7 INTRODUCTION .................................................................................................................. 7 REVIEW OF PAST WORK.................................................................................................... 8 Conclusion from literature ............................................................................................ 12 Work done in this semester ................................................................................................. 13 Experiment work .............................................................................................................. 13 MATLAB Programming .................................................................................................... 15 MODELLING IN OLIVE LAB TERRAIN ........................................................................... 18 Comparison of results with experimental results .............................................................. 22 Future Work ........................................................................................................................ 23 References ...................................................................................................................... 23 ~5~
  • 6. LIST OF TABLES & FIGURES Table 1 Literature related to insertion losses in a barrier sorted based on the parameters being varied .......................................................................................................................... 9 Figure 1 Noise barriers with various shape edges and surface conditions............................. 8 Figure 2 Schematic of the experiment performed ................................................................ 13 Figure 3 Experimental Setup for the soft ground ................................................................ 13 Figure 4 Experiment setup for hard ground ......................................................................... 14 Figure 5Definitions of symbols used to determine Fresnel Number ‘N’ ................................ 15 Figure 6Paths considered in Lam Method ........................................................................... 16 Figure 7 Flowchart of the matlab code ................................................................................ 16 Figure 8 Matlab GUI ............................................................................................................ 17 Figure 9 Comparison of insertion losses with change in height at different frequencies ...... 18 Figure 10Comparison of insertion losses with frequency variation at different heights ........ 19 Figure 11 Variation of thickness .......................................................................................... 20 Figure 12 a) single panel barrier b) double panel barrier ......................................... 20 Figure 13 IL variation in single and double panels (frequency=1000hz) .............................. 21 Figure 14 IL variation in single and double panels (frequency=2000hz) .............................. 21 Figure 15Comparision of matlab and software results with experimental results at 500 Hertz ........................................................................................................................................... 22 Figure 16Comparisonof MATLAB and software results with Experimental results at 1000 Hertz ................................................................................................................................... 22 ~6~
  • 7. PROBLEM STATEMENT AND MOTIVATION Specific Aim: To design an effective and cost-efficient noise barrier for the baffle range which can reduce the unwanted noise up to the required level. Usually firing ranges where soldiers are trained for the shooting at different conditions are made out of the city so that there was no disturbance to the local residents. But some of the ranges are within the residential areas where common people feel a lot of noise. So, to get the control over this type of noise a noise barrier need to be designed around the range to reduce the noise up to a desirable level. INTRODUCTION Increasing noise pollution will lead to an ever increasing need to control noise of all forms. Noise barriers are the most common solution for controlling noise from surroundings and several methods have been developed for improving their efficiency without increasing their height. Examples of already deployed noise barriers in India: 1. Noise Barriers in BKC, Mumbai (2010) 2. IIT Powai noise barrier (2012) 3. Commonwealth Games noise barrier (2010) 4. Sound barriers at Suman Nagar, Navghar flyovers (2012) The vast majority of these have been vertical, reflective wall made of concrete, wood or steel. The standard top for these walls is a “knife-edge”, providing a single diffraction edge with a reflective diffraction zone. Clearly, there are many other options for noise barrier shapes than vertical reflective walls with knife-edge diffraction zone. In addition to it, there are option to make barriers absorptive, to displace the diffraction zone through the use of a slanted section on top, or to provide for a double- diffraction zone through the use of a T-top section and other modified tops of the walls. ~7~
  • 8. REVIEW OF PAST WORK During summer internship most of the literature work was performed and all the work is presented in the tabular form in table 1 and table 2. During this time also complete study was performed and the entire phenomenon was studied. Different types of barrier that were studied are: - Shaped Barrier - Conventional Barrier - T-shaped barrier - Multiple Edge Barrier - Arrow shape Barrier Figure 1 illustrates various noise barriers obtained by varying the shape edges and surface conditions. FIGURE 1: NOISE BARRIERS W ITH VARIOUS SHAPE EDGES AND SURFACE CONDITIONS ~8~
  • 9. TABLE 1LITERATURE RELATED TO INSERTION LOSSES IN A BARRIER SORTED BASED ON THE PARAMETERS BEING VARIED Different barrier Simple T-top y-top Cylindrical Wedge Multipl Angled edge Parameter top shaped e edge Barrier height D. C. David J. HOTHERSA Oldham , LL, S. N. Christopher A. CHANDLER Egan (2011) -WILDE AND M. N. P.J. Thorsson HAJMIRZAE (2003) (1990) Takashi Ishizuka*, Kyoji Fujiwara (2003) Change in David J. D J Oldham and C A Egan source position Oldham , (2009) Christopher A. Egan (2011) D. C. D. C. D. C. HOTHERSA HOTHERSALL HOTHER Receiver height LL, S. N. , S. N. SALL, S. CHANDLER CHANDLER- N. -WILDE WILDE AND CHANDL AND M. N. M. N. ER- HAJMIRZAE HAJMIRZAE(1 WILDE (1990) 990) AND M. N. HAJMIR ZAE(1990 ) Change in A. Muradali David J. D. C. C.A. receiver and K. R. Oldham , HOTHER Egan, V position Fyfe (1994) Christopher A. SALL, S. Chilekw Egan (2011) N. a and D. D. C. D. C. CHANDL J. HOTHERSA Hothersall, D. ER- Oldham LL, S. N. H. Crombie & WILDE (2006) CHANDLER S. N. Chandler- AND M. -WILDE Wilde N. AND M. N. HAJMIR HAJMIRZAE C.A. Egan, V ZAE(1990 (1990) Chilekwa and ) D. J. Oldham(2006) D. C. HOTHERSALL , S. N. CHANDLER- WILDE AND M. N. ~9~
  • 10. HAJMIRZAE(1 990) Width of top David J. D. H. Oldham , Crombi Christopher A. e, D. C. Egan (2011) Hothers all& S. D. C. N. Hothersall, D. Chandle H. Crombie & r-Wilde S. N. Chandler- (1994) Wilde C.A. Egan, V C.A. Egan, V Chilekw Chilekwa and a and D. D. J. J. Oldham(2006) Oldham (2006) Cap depth D. C. TomonaoO D. H. Hothersall, D. kuboa) and Crombi H. Crombie & Kyoji e, D. C. S. N. Chandler- Fujiwara Hothers Wilde all& S. P.J. Thorsson N. (2003) Chandle r-Wilde (1994) D. C. D J Oldham and C A Egan Angle variation HOTHER (2009) SALL, S. N. CHANDL ER- WILDE AND M. N. HAJMIR ZAE(1990 ) D. C. Takashi Hothersall, D. Takashi D. C. Takashi Takashi Ishizuka*, Kyoji Comparison Ishizuka*, H. Crombie & Ishizuka*, HOTHER Ishizuka Fujiwara (2003) with T-top Kyoji S. N. Chandler- Kyoji SALL, S. *, Kyoji Fujiwara Wilde(1990) Fujiwara N. Fujiwar (2003) (2003) CHANDL a (2003) Takashi ER- D. C. Ishizuka*, WILDE HOTHERSA Kyoji Fujiwara AND M. LL, S. N. (2003) N. CHANDLER HAJMIR -WILDE ZAE AND M. N. (1990) HAJMIRZA E (1990) ~ 10 ~
  • 11. barrier surface David J. David J. D. C. D. H. D J Oldham and C A Egan variation Oldham , Oldham , HOTHER Crombi (2009) Christopher Christopher A. SALL, S. e, D. C. A. Egan Egan (2011) N. Hothers (2011) CHANDL all& S. D. C. P.J. Thorsson ER- N. HOTHERSA (2003) WILDE Chandle LL, S. N. AND M. r- CHANDLER N. Wilde(1 -WILDE HAJMIR 994) AND M. N. ZAE(1990 HAJMIRZA ) E(1990) top surface David J. D. C. D. H. D J Oldham and C A Egan absorption Oldham , Hothersall, D. Crombi (2009) variation Christopher A. H. Crombie & Takashi e, D. C. Egan (2011) S. N. Chandler- Ishizuka*, Hothers Wilde (1990) Kyoji all& S. D. C. Fujiwara N. Hothersall, D. (2003) Chandle H. Crombie & r- S. N. Chandler- Wilde(1 Wilde 994) C.A. Egan, V C.A. Chilekwa and Egan, V D. J. Chilekw Oldham(2006) a and D. J. D. C. Oldham HOTHERSALL (2006) , S. N. CHANDLER- WILDE AND M. N. HAJMIRZAE(1 990) M.R. Monazzam, Y.W. Lam(2006) Ground surface Muradali and D. C. variation K. R. Fyfe Hothersall, D. (1994) H. Crombie & S. N. Chandler- D. C. Wilde HOTHERSA LL, S. N. P.J. Thorsson CHANDLER (2003) -WILDE AND M. N. HAJMIRZA E(1990) ~ 11 ~
  • 12. MahdiyehNader Perforated zadeh a,⇑, sheet on Mohammad diffuser Reza Monazzam b, ParvinNassiri b, SamanehMome nBellahFard (2011) QRD on top M.R. Monazzam, Y.W. Lam(2006) MahdiyehNader zadeh a,⇑, Mohammad Reza Monazzam b, ParvinNassiri b, SamanehMome nBellahFard(20 11) Soft TomonaoO kuboa) and Kyoji Fujiwara Reflective top D. H. D J Oldham and C A Crombi Egan(2009) e, D. C. Hothers all& S. N. Chandle r- Wilde(1 994) CONCLUSION FROM LITERATURE Going through all the research papers and by seeing their comparative study, it was vaguely suggested that T-type barrier having absorptive coating suits best to get maximum sound abatement. Since for a single barrier height/cost ration peaks at 3meter so height of T-top barrier should be taken 3meter and width of the top can be taken as 1 meter so that aesthetically is looks good and having maximum sound abatement. Till internship the project was not having any practical touch and in this research paper experiments were conducted and results was compared to get the real and practical touch ~ 12 ~
  • 13. WORK DONE IN THIS SEMESTER EXPERIMENT WORK SCHEMATIC FIGURE 2: SCHEMATIC OF THE EXPERIMENT PERFORMED Figure 2 shows the basic schematics of the experiments that were performed and it shows various parameter that is involved during calculations. EXPERIMENT ON SOFT GROUND FOR AN EXISTING WALL FIGURE 3 : EXPERIMENTAL SETUP FOR THE SOFT GROUND ~ 13 ~
  • 14. Figure 3 shows the experiment that was performed on an existing wall at the fuel-zap in IIT Ropar to get the basic insight of the insertion loss values obtained. The material of the wall is concrete with a height of 170 cm and thickness of 22 cm. The parameters that are varied in this experiment are frequency (varied between 100-1000Hz at an interval of 100 Hz) and receiver distance (varied between 3-15m from the wall) while keeping all other parameters constant. The source height and receiver height are kept in the shadow region with values of 50 cm and 100 cm respectively. EXPERIMENT ON HARD GROUND FIGURE 4EXPERIMENT SETUP FOR HARD GROUND The experiment was performed on a finite barrier on hard ground to enable comparisons as most of the analytical solutions are for hard ground. Figure 4 shows the experimental setup of the experiment. The material of the barrier is wood with a height of 90 cm, width of 108 cm and thickness of 2 cm. The parameters that are varied in this experiment are frequency (varied between 100-1000Hz at an interval of 100 Hz) and receiver distance (varied between 0-16m from the barrier) while keeping all other parameters constant. The source height and receiver height are kept in the shadow region with values of 50 cm and 83 cm respectively. ~ 14 ~
  • 15. MATLAB PROGRAMMING THEORY: LAM’S METHOD USING MAEKAWA’S CURVE Maekawa introduced an empirically based diffraction model that provides the insertion loss due to a thin-walled barrier in terms of the Fresnel number.Maekawa then suggested that the insertion loss for a finite-length barrier could be determined by multiple application of this curve to the diffraction paths around the barrier and then summing the energy contributions of these paths. Maekawa‟s curve can be represented by the following two equations: where N is Fresnel Number given by Where (A+B-d) is the path difference and λ is the wavelength. The symbols are defined as shown in the Figure 5. FIGURE 5 DEFINITIONS OF SYMBOLS USED TO DETERMINE FRESNEL NUMBER ‘N’ Lam improved on Maekawa‟s method by summing complex pressures, instead of energies, of each diffraction path around the barrier. This was done to incorporate the phase interaction and interference between the paths, the absence of which, Lam suggested, was the cause of the poor agreement between Maekawa‟s method and experimental results. A semi-infinite barrier is equivalent to a 2D geometry. Diffraction Paths considered for a semi-infinite thin barrier are as shown in Figure 6. ~ 15 ~
  • 16. FIGURE 6 PATHS CONSIDERED IN LAM METHOD The barrier insertion loss is given by: Mi represents the insertion loss value from Maekawa‟s curve for the ithpath. The subscript „o‟ refers to the direct path (from the source to receiver) and the subscript „r‟ refers to the ground reflected path (from the source image to receiver). The Lam method fell short when the receivers were in the proximity of the line-of-sight, and when parallel geometries in 2D were considered. This is due to the fact that this method does not predict a unique phase shift at the diffraction edge for each path. GUI IMPLEMENTATION FIGURE 7: FLOWCHART OF THE MATLAB CODE ~ 16 ~
  • 17. A MATLAB GUI has been made for calculating the insertion loss. It includes analysis for an input data. A GUI (graphical user interface) allows users to perform tasks interactively through controls such as buttons and sliders. Within MATLAB®, GUI tools enable you to perform tasks such as creating and customizing plots, fitting curves and surfaces, and analyzing and filtering signals. Figure 8 shows the typical GUI that was modeled in the Matlab using Lam‟s equation. Parameters that were involved in GUI are barrier height, Source and receiver height, source and receiver distance, and frequency of the sound. It also shows the graphical variation of the variation in one parameter by taking 5 other parameter constant and vary 6th one. FIGURE 8 MATLAB GUI ~ 17 ~
  • 18. MODELLING IN OLIVE LAB TERRAIN ABOUT THE SOFTWARE THEORY The acoustic calculations are made by the software based on Hadden& Pierce Diffraction 3D model implemented with finite impedances faces using Salomons semi-analytical method including ground effects. Multiple barrier diffraction is calculated in a recursive way at any diffraction order.Ground effect is included using the One Parameter Theory of Chessell based on Delany and Bazley. LIMITATIONS The thickness of the barrier cannot be reduced to a value less than 3cm. The numerical values of the readings are available only at octave and 1/3rd octave frequencies. Any other parameter except frequency cannot be varied in the same model. ANALYSIS MADE VARIATION OF HEIGHT PARAMETERS Barrier Material: mineral wool Barrier type: Thin Barrier Receiver Height= 50 cm Source Height= 50cm Source distance=5m 35 30 Insertion Loss(in dB) 25 20 1000 Hz 15 1995 Hz 10 3981 Hz 5 0 0 1 2 3 4 5 Barrier height(in m) FIGURE 9: COMPARISON OF INSERTION LOSSES WITH CHANGE IN HEIGHT AT DIFFERENT FREQUENCIES ~ 18 ~
  • 19. 35 30 25 Insertion Loss(in dB) 20 h=1m h=2m 15 h=3m 10 h=4m 5 0 2 2.5 3 3.5 4 -5 log(frequency(in Hz)) FIGURE 10: COMPARISON OF INSERTION LOSSES WITH FREQUENCY VARIATION AT DIFFERENT HEIGHTS It can be seen that the insertion loss increases with increase of barrier height. From the figure 7, it can be seen that the variation of the insertion loss values is not much when it is changed from a height of 3m to 4m. VARIATION OF THICKNESS MASS LAW When sound is incident upon a wall or partition, some of it will be reflected and some will be transmitted through the wall. The transmission loss obtained can be determined using mass law at a particular frequency. Where m=mass density and f=frequency PARAMETERS Barrier Material: mineral wool Flow resistivity=20000 Pas/m2 Barrier Height = 2m Receiver Height= 1 m Source Height = 1 m Source distance=2m ~ 19 ~
  • 20. Frequency=1500 Hz 30 25 20 Insertion Loss(in dB) thickness_3cm 15 thickness_3.5cm thickness_4cm 10 thickness_4.5cm 5 0 0 10 20 30 40 50 60 -5 Receiver distance (in m) FIGURE 11 VARIATION OF THICKNESS From figure 8 it can be clearly seen that the value of insertion loss doesn‟t vary much with the receiver distance for thickness values greater than the optimum value calculated from the mass law (≈2.5cm). SINGLE VS DOUBLE PANELS FIGURE 12 A) SINGLE PANEL BARRIER B) DOUBLE PANEL BARRIER PARAMETERS Barrier Material: mineral wool Flow resistivity 20000 Pas/m2 Barrier Height 2m Barrier Thickness 20cm single 10 cm double Receiver Height 1m Source Height 1m Source distance 2m ~ 20 ~
  • 21. 45 Frequency = 1000 Hz 40 35 single panel 30 25 double Insertion Loss(in dB) 20 panel_gap20cm 15 double panel_gap 30cm 10 5 double panel_gap50cm 0 0 2 4 6 8 10 12 Receiver distance(in m) FIGURE 13 IL VARIATION IN SINGLE AND DOUBLE PANELS (FREQUENCY=1000HZ) 45 40 35 Frequency = 2000 Hz Insertion Loss(in dB) 30 single panel 25 double panel gap 20 20 cm double panel_gap 15 30cm 10 double panel_gap50cm 5 0 0 2 4 6 8 10 12 Receiver distance (in m) FIGURE 14 IL VARIATION IN SINGLE AND DOUBLE PANELS (FREQUENCY=2000HZ) From the figures 13 and 14 it can be clearly seen that double panel barriers are more effective in sound reduction compared to single panel barrier and the insertion loss increases with increase in gap between the two panels. ~ 21 ~
  • 22. COMPARISON OF RESULTS WITH EXPERIMENTAL RESULTS PARAMETERS Barrier Material: wood Barrier Height=90 cm Barrier Width=105 cm Barrier Thickness= 2cm Receiver Height= 80 cm Source Height= 50 cm FIGURE 15 COMPARISION OF MATLAB AND SOFTWARE RESULTS WITH EXPERIMENTAL RESULTS AT 500 HERTZ FIGURE 16COMPARISONOF MATLAB AND SOFTWARE RESULTSWITH EXPERIMENTAL RESULTSAT 1000 HERTZ From the figures 15 and 16 it can be seen that the results from the software are in coherence with those of the experimental results within acceptable error limits. It can also be seen there is a considerable variation in the results obtained from MATLAB program, the reasons of which can be attributed to the assumptions made in the theoretical model, where it considers the barrier is semi-infinite with negligible thickness and which doesn‟t include the effect of the material of the barrier. ~ 22 ~
  • 23. FUTURE WORK Some part of the project is completed in B.Tech-1 project which was in this semester and this project will be continued in coming semester also as B.Tech-2 project. The things which are planned for coming semester are: 1. In current work, Material selection for the barrier was not suggested so work will be done in this context in the upcoming semester. 2. In current work, output from the software of single and double panels was compared but there physical modelling was not done. It will be includedin the further studies. 3. The software which is presently used has certain limitations due to which one cannot vary the shape of the barrier. The new software SYSNOISE, which is BEM/FEM software, was purchased for getting more accurate results and help in physical modelling of the system. 4. In current study the MATLAB formulations are donefor a semi-infinite, thin barrier. In 2nd part the more focus will be made in including parameters like thickness, finiteness, etc. 5. In our next work formation of the optimization problem will be included and will be solved using different optimization techniques. REFERENCES Web site reference 1. http://sciencedirect.com/ 2. http://www.acoustax.com/noise-barrier-specs.php 3. http://www.acousticalsurfaces.com/wall_barrier/wall_barrier.htm 4. http://www.nrc-cnrc.gc.ca/eng/ibp/irc/bsi/85-sound-tranmission.html 5. http://articles.timesofindia.indiatimes.com/2012-05-17/mumbai/31747986_1_noise- barrier-noise-levels-sumaira-abdulali 6. http://www.nrc-cnrc.gc.ca/eng/ibp/irc/bsi/85-sound-tranmission.html 7. http://www.otlterrain.com/ Research Papers [1] R.O.Feher, proc.Ann.Nat. Noise Abatement Symp.,1951,p-98 [2] A.Muradali and K.R Fyfe,A study of 2d and 3d barrier insertion loss using improved diffraction based methods, applied acoustics,vol.53,no-1-3,pp 49-75,1998 [3] D. C. HOTHERSALL, S. N. CHANDLER-WILDE AND M. N. HAJMIRZAE, Efficiency of Single Noise barrier, Journal of Sound and Vibration (1991) 146(2), 303-322. ~ 23 ~
  • 24. [4] David J. Oldham , Christopher A. Egan.. A parametric investigation of the performance of T-profiled highway noise barriers.. Applied Acoustics 72 (2011) 803–813 [5] C.A. Egan, V Chilekwa and D. J. Oldham, Top edge treatment to enhance the performance of a noise,Acoustics Research Unit, University of LiverpoolLiverpool, L69 3BX, United Kingdom [6] Watts, G.R., Barrier design to reduce road traffic noise. Proceedings of the Institution of Civil Engineers, 2002. 53(2): p. 79- 86. [7] Takashi Ishizuka, KyojiFujiwara,Performance of noise barriers with various edge shapes and acoustical conditions.. Applied Acoustics 65 (2004) 125–141. [8] MahdiyehNaderzadeh, Mohammad Reza Monazzam, ParvinNassiri, SamanehMomenBellahFard, Application of perforated sheets to improve the efficiency of reactive profilednoise barriers, Applied Acoustics 72 (2011) 393–398. [9] A. Muradali and K. R. Fyfe, A Study of 2D and 3D Barrier Insertion Loss using Improved Diffraction-based Methods, Applied Acoustics, Vol. 53, No. I-3, pp. 49- 15, 1998 [10] Maekawa, Z., Noise reduction by screens. Applied Acoustics, 1968, 1, 157- 173. [11] Pontus J. Thorsson,Combined effects of admittance optimisationon both barrier and ground, Applied Acoustics 64 (2003) 693–711. [12] D J Oldham and C A Egan, The development of a practical top edge device for a noise barrier, 16th international congress on noise and vibration July 2009. ~ 24 ~