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The	Enhancement	of	Convec/ve	
Heat	Transfer	in	an	Aluminum	Oxide	
Nanoaerosol	
Empirical	Study	
Maulin	Trivedi	
Dec	9,	2015	
	
Mechanical	and	Manufacturing	Engineering
Applica/ons	
§  Deep-cooled	combined	
turbojet	cycle	
—  Thrust	over	wide	range	of	Mach	
number	
—  Intake	air	has	very	high	
temperature	
—  Energy	extracted	is	added	back	
to	fuel	stream	
§  Heat	transfer	applica/ons	use	
fluids	or	air	as	heat	carriers.	
—  Thermal	constraints	
—  Physical	constraints	
—  Cost	
2	
Figure	1:	DASS	GN	1	Engine	Concept	
From:	h(ps://en.wikipedia.org/wiki/Space_Engine_Systems
Applica/ons	
§  Heat	transfer	applica/ons	use	
fluids	or	air	as	heat	carriers.	
— Thermal	constraints	
— Physical	constraints	
— Cost	
§  Reac/on	Engines	Ltd.	
— High	surface	area	
§  Space	Engine	Systems	
— Enhanced	thermal	proper/es	
Figure	2:	SABRE	Pre-cooler	
From:	
h(p://www.reac;onengines.co.uk/heatex_work.html	
3
Background	
§  Solid	par/cles	in	suspension	increases	thermal	conduc/vity	
(Maxwell,	1881).	
— Mass	or	volume	frac/on	of	par/cles	
— Surface	area	to	volume	ra/o	
§  Nanopar/cles	
— Sizes	1	-	100nm	
— Very	high	surface	area	to	volume	ra/o	
§  Nanofluids:	Nanopar/cles	suspended	in	liquid	phase	carriers	(Choi,	
1995).	
§  Nanoaerosols:	Nanopar/cles	suspended	in	gaseous	phase	carriers.	
4
Background:	Nanofluids	
§  40%	heat	transfer	
enhancement	(Heris	et	
al.,	2006).			
§  39%	increase	in	heat	
transfer	(Xuan	et	al.,	
2003).	
§  Dependency	on	mass	
frac/on	and	Reynolds	
number	
Figure	3:	Nusselt	number	vs	Peclet	number	
From:	
Heris,	S.	Z.,	Etemad,	S.	G.,	&	Esfahany,	M.	N.	(2006).	Experimental	
inves/ga/on	of	oxide	nanofluids	laminar	flow	convec/ve	heat	transfer.	
Interna;onal	Communica;ons	in	Heat	and	Mass	Transfer,	33(4),	529-535.	
	
5
Background:	Nanoaerosol	
Figure	4:	Nusselt	number	vs	mass	loading		 Figure	5:	Nusselt	number	vs	par/cle	size	
Adapted	from:	Murray,	D.	B.	(1994).	Local	enhancement	of	heat	transfer	in	a	par/culate	cross	flow—II	Experimental	data	and	predicted	trends.	
Interna;onal	journal	of	mul;phase	flow,	20(3),	505-513.	
	
6
Background:	Mechanisms	
§  Increased	thermal	capacity	
§  Conduc/on	between	impac/ng	par/cles	
§  Thermal	energy	transport	by	rebounding	par/cles	
§  Flow	structure	effects	
§  Other	effects	(Williams,	2015)	
§  Limi/ng	mechanisms	
7
Mo/va/on	
§  Nanopar/cles	vs.	Micro-par/cles	
§  Availability	in	aerospace	industry	as	an	alterna/ve	fuel	
— Large	energy	content	per	unit	volume	and	mass	
— Lower	igni/on	temperatures	and	higher	burning	rate	
— Safe	and	efficient	storage	
§  Nanofluids	are	proven	effec/ve	in	heat	transfer	applica/ons	
§  Volumetric	heat	capacity	of	nanoaerosol	is	much	higher	compared	
to	nanofluids	
— ρCp	ra/o	is	much	higher	for	nanoaerosol	than	for	nanofluids	
8
Objec/ves	
§  First	experimental	inves/ga/on	
§  Low	par/cle	concentra/on	
— Mass	frac/on	for	nanofluids,	O(10-1)	
— Mass	frac/on	for	nanoaerosols,	O(10-4)	
§  Theore/cal	model	to	predict	enhancement	
§  Par/cle	size	vs.	heat	transfer	enhancement	
9
Experimental	Set-up:	Cont.	
10	Figure	6:	Experimental	Schema/c
Experimental	Set-up:	Cont.	
11	Figure	6:	Experimental	Schema/c	
Hot-Wire	 Flow
Experimental	Set-up	
12	Figure	7:	Experimental	Set-up	
Pressure	Regulator	
Compressed	Air	
Pressure	
Gauge	
Flow	
Meter	
Par/cle	
Injector	
Upstream	
Thermistor	
Hot	
Wire	
Downstream	
Thermistor	
Par/cle	Collec/on	Tank
Air-only	Tests	
§  Validate	experimental	apparatus	
§  Performed	over	flow	Reynolds	number	range	of	1420	-	11,200	
§  Nusselt	number	calculated	by	equa/ng	convec/ve	heat	
transfer	rate	to	the	change	in	enthalpy	
§  Experimental	results	(without	par/cles)	were	compared	to	
Zukauskas	empirical	rela/on	of		
§  Establish	base	line	
13
Air-only	Tests:	Cont.	
14	
0	
2	
4	
6	
8	
10	
12	
14	
16	
18	
20	
0	 2000	 4000	 6000	 8000	 10000	 12000	
Nusselt	Number	
Reynolds	Number	[tube	diameter],	Re	
Zukauskas	Rela/on	
Experimental	Air	Tests	
Figure	8:	Valida/on	of	experimental	set-up
Air	Tests:	Cont.	
15	
0	
2	
4	
6	
8	
10	
12	
14	
16	
18	
20	
0	 2000	 4000	 6000	 8000	 10000	 12000	
Nusselt	Number	
Reynolds	Number	[wire	diameter],	Re	
Zukauskas	Rela/on	
Experimental	Air	Tests	
Figure	8:	Valida/on	of	experimental	set-up	
Flow	Condi/ons	For	Par/cle	Tests
Nanopar/cle:	Informa/on	
§  Approximately	spherical	
with	112	nm	avg.	dia.	
§  Agglomerates	of	avg.	
870	nm.	
§  Dispersed	through	
custom-built	injec/on	
system.	
	
16	
Figure	9:	SEM	image	of	Al2O3	par/cles
Nanopar/cle:	Injec/on	System	
§  Gravity	assisted	through	
orifice	of	0.75	mm	
§  Oscilla/ons	provided	to	
prevent	clogging	
§  510	mm	of	tubing	
allows	semling	of	bigger	
par/cles	
17	
Figure	10:	Par/cle	Injec/on	System	
Par/cle	Housing	
Off-balance	Motor	
Air-flow	pipe	
Upstream	
Thermistor
Par/cle	Tests	
§  Experiments	with	par/cles	were	performed	at	flow	Reynolds	
numbers:	6000,	7500	and	8900.		
§  Par/cle	flow	rate	measured	aner	each	test	using	highly	
sensi/ve	mass	balance.	
§  Par/cle	mass	loading	ranged	from	0.01%-0.33%.	
§  Nusselt	number	at	each	Reynolds	number	calculated	using	
same	methodology	as	air	tests.	
— Effec/ve	proper/es	
18
Experimental	Results:	Cont.	
19	
Figure	11:	Effect	of	mass	loading	on	Nu	at	Re	=	6000	
y	=	9.5795x0.5809	
R²	=	0.70653	
0%	
5%	
10%	
15%	
20%	
25%	
30%	
35%	
40%	
45%	
0.00%	 0.05%	 0.10%	 0.15%	 0.20%	 0.25%	 0.30%	 0.35%	
%Nu	Increase	
%Par/cle	Mass	Loading	
Raw	%Nu	Increase	 Predicted	%Nu	Increase	 95%	Lower	CI	 95%	Upper	CI
Experimental	Results:	Cont.	
20	
Figure	12:	Effect	of	mass	loading	on	Nu	at	Re	=	7500	
y	=	5.3126x0.5338	
R²	=	0.61755	
0%	
5%	
10%	
15%	
20%	
25%	
30%	
35%	
40%	
0.00%	 0.05%	 0.10%	 0.15%	 0.20%	 0.25%	 0.30%	 0.35%	
%Nu	Increase	
%Par/cle	Mass	Loading	
Raw	%Nu	Increase	 Predicted	%Nu	Increase	 95%	Lower	CI	 95%	Upper	CI
Experimental	Results:	Cont.	
21	
Figure	13:	Effect	of	mass	loading	on	Nu	at	Re	=	8900	
y	=	0.9927x0.2821	
R²	=	0.46192	
0%	
5%	
10%	
15%	
20%	
25%	
30%	
35%	
40%	
0.00%	 0.05%	 0.10%	 0.15%	 0.20%	 0.25%	 0.30%	 0.35%	
%Nu	Increase	
%Par/cle	Mass	Loading	
Raw	%Nu	Increase	 Predicted	%Nu	Increase	 95%	Lower	CI	 95%	Upper	CI
Error	Analysis	
§  Systema/c	errors	calculated	
based	on	instrumenta/on	and	
sensor	limita/ons.	
§  Random	errors	calculated	based	
on	t-distribu/on	for	α	=	0.05.	
§  Random	error	is	significantly	
higher	than	systema/c	errors.		
§  Student’s	t-test	between	baseline	
test	and	par/cle	test	at	lowest	
par/cle	concentra/on	shows	
significant	increase	in	Nusselt	
number.	
22	
9	
10	
11	
12	
13	
14	
15	
16	
17	
550	 600	 650	 700	 750	 800	 850	 900	 950	
Nusselt	Number	
Cross-flow	Reynolds	Number	
Air	Test	 Par/cle	Test	
Figure	 14:	 Student's	 t-test	 for	 95%	 confidence	
between	air-only	and	lowest	par/cle	loading	tests
Model:	Con/nuum	
§  Con/nuum	regime,	Kn	<	0.01	
— Murray’s	model	for	increased	thermal	capacity	
— ​(​​ 𝑁 𝑢↓𝑁𝐴 /​ 𝑁 𝑢↓𝑎  )↓𝐼𝑇𝐶 =​[1+​ 𝜂↓𝑡 ​ 𝑆↓𝐿 ​​ 𝑐↓𝑝 ↓𝑟𝑎𝑡𝑖𝑜 ]↑0.37 	
§  ​ 𝜂↓𝑡 =​​ 𝜏↓𝑟𝑒𝑠 /​ 𝜏↓𝑟𝑒𝑙  ;			​ 𝜏↓𝑟𝑒𝑙 =​​ 𝑑↓𝑝 ​ 𝜌↓𝑝 ​​ 𝑐↓𝑝 ↓𝑝 /​6ℎ↓𝑝  	
§  Other	effects	are	considered	negligible	due	to	low	par/cle	
loading	
— Flow	structure	modifica/on	
— Par/cle	rebound	
— Radia/on	
23
Model:	Free-molecular	
§  Free-molecular	regime,	Kn	>	10	
— Modified	Murray’s	model	using	the	free-molecular	
relaxa/on	/me,	τrel	
— Obtained	from	Filippov	and	Rosner’s	energy	balance	
§  ​ 𝜌↓𝑝 ​ 𝐶↓​ 𝑝↓𝑝  ​ 𝑉↓𝑝 ​ 𝑑​ 𝑇↓𝑝 /𝑑𝑡 = 𝛼𝜋​ 𝑎↑2 ​ 𝑛↓𝑔 ​ 𝑐 ​ 𝑘↓𝑏 (​1/2 (​ 𝑇↓𝑝 −​
𝑇↓𝑔 )(​ 𝛾+1/𝛾−1 )) 	
§  ​ 𝜏↓𝑟𝑒𝑙 =​2​ 𝜌↓𝑝 ​ 𝑐↓𝑝 ​ 𝑑↓𝑝 /9​ 𝑛↓𝑔 ​ 𝑐 ​ 𝑘↓𝑏  ;	​ 𝑛↓𝑔 =​ 𝑃​ 𝑁↓𝑎𝑣 /𝑅𝑇 ;	​ 𝑐 
=√⁠​8​ 𝑘↓𝑏 ​ 𝑇↓𝑔 /𝜋​ 𝑚↓𝑔   	
— Subs/tute	τrel	into	Murray’s	model	to	obtain	Nusselt	
number	enhancement	
24
Model:	Transi/on	
§  Transi/on	regime,	0.01	<	Kn	<	10	
— Harmonic	mean	suggested	by	Sherman	(1963)	was	used	to	
interpolate	​​ 𝑞↓𝑡𝑟  .	
— ​ 𝜏↓𝑟𝑒𝑙, 𝑡𝑟 =​​ 𝜌↓𝑝 ​ 𝑐↓𝑝 ​​ 𝑑↓𝑝 ↑2 /​​​ 𝑞↓𝑡𝑟  /​​ 𝑞↓𝑐   12​ 𝑘↓𝑓  ;		​​​ 𝑞↓𝑡𝑟  /​​
𝑞↓𝑐   = ​1/1+​19/6 𝐾𝑛 	
— The	ra/o	​​​ 𝑞↓𝑡𝑟  /​​ 𝑞↓𝑐   	can	be	obtained	from	Liu	(2006).	
— Knudsen	number	effects	are	incorporated	into	the	
/mescale	
25
Model:	Comparison	
26	
1.00	
1.10	
1.20	
1.30	
1.40	
1.50	
1.60	
1.70	
1.80	
1.90	
0.00%	 0.05%	 0.10%	 0.15%	 0.20%	 0.25%	 0.30%	 0.35%	
Nu	Ra/o	[Nu_su/Nu_a]	
Solid	Mass	Frac/on,	%	[m_solid/m_air	*100]	
Experimental	Fit	 Experimental	Data	 Transi/onal	Model	
Murray	Model	 Free	Molecular	Model	 95%	Confidence	Band	
Figure	15:	Comparison	of	con;nuum	model,	free-molecular	model,	transi;onal	
model	and	experimental	data	for	Re	=	6000
27	
1.00	
1.10	
1.20	
1.30	
1.40	
1.50	
1.60	
1.70	
1.80	
1.90	
0.00%	 0.05%	 0.10%	 0.15%	 0.20%	 0.25%	 0.30%	 0.35%	
Nu	Ra/o	[Nu_su/Nu_a]	
Solid	Mass	Frac/on,	%	[m_solid/m_air	*100]	
Experimental	Fit	 Experimental	Data	 Transi/onal	Model	
Murray	Model	 Free	Molecular	 95%	Confindence	Band	
Figure	16:	Comparison	of	con;nuum	model,	free-molecular	model,	transi;onal	
model	and	experimental	data	for	Re	=	7500	
Model:	Comparison
28	
1.00	
1.10	
1.20	
1.30	
1.40	
1.50	
1.60	
1.70	
1.80	
1.90	
0.00%	 0.05%	 0.10%	 0.15%	 0.20%	 0.25%	 0.30%	 0.35%	
Nu	Ra/o	[Nu_su/Nu_a]	
Solid	Mass	Frac/on,	%	[m_solid/m_air	*100]	
Experimental	Fit	 Experimental	Data	 Transi/onal	Model	
Murray	Model	 Free	Molecular	Model	 95%	Experimental	Band	
Figure	17:	Comparison	of	con;nuum	model,	free-molecular	model,	transi;onal	
model	and	experimental	data	for	Re	=	9000	
Model:	Comparison
Model:	Effect	of	Par/cle	Size	
29	
1.00	
2.00	
3.00	
4.00	
5.00	
6.00	
7.00	
8.00	
9.00	
10.00	
0	 10	 20	 30	 40	 50	 60	 70	 80	 90	 100	
Nusselt	Number	Ra/o	
Par/cle	Diameter,	[nm]	
Solid	Loading	0.25%	 Solid	Loading	0.5%	 Solid	Loading	0.75%	 Solid	Loading	1%	
Figure	18:	Effect	of	par/cle	size	on	Nusselt	number	ra/o	at	Re	=	9000	using	
transi/onal	model
Discussion:	Experimental	
§  Only	small	par/cle	mass	loading	is	required	
to	provide	a	large	increase	to	Nusselt	
number.	
§  Murray	(1994)	required	~100%	mass	
loading	to	achieve	similar	results.	
§  Higher	enhancement	amributed	to:	
— Smaller	par/cles	
— Lower	Reynolds	number	
30	
From:	Murray,	D.	B.	(1994).	
Local	enhancement	of	heat	
transfer	in	a	par/culate	
cross	flow—II	Experimental	
data	and	predicted	trends.	
Interna;onal	journal	of	
mul;phase	flow,	20(3),	
505-513.
Discussion:	Experimental	
§  Only	small	par/cle	mass	loading	is	required	
to	provide	a	large	increase	to	Nusselt	
number.	
§  Murray	(1994)	required	~100%	mass	
loading	to	achieve	similar	results.	
§  Higher	enhancement	amributed	to:	
— Smaller	par/cles	
— Lower	Reynolds	number	
31	
From:	Murray,	D.	B.	(1994).	
Local	enhancement	of	heat	
transfer	in	a	par/culate	
cross	flow—II	Experimental	
data	and	predicted	trends.	
Interna;onal	journal	of	
mul;phase	flow,	20(3),	
505-513.
Discussion:	Model	
§  Effects	of	increased	Reynolds	number	and	turbulence	
modifica/on	are	insignificant.	
§  The	relaxa/on	/me	represents	63%	of	heat	transfer,	thus	
resul/ng	in	higher	predic/on	of	heat	transfer	enhancement.	
§  Experimental	data	between	con/nuum	and	free-molecular	
predic/on.	
§  Transi/onal	model	agrees	with	experimental	data.	
— For	0.01	<	Kn	<	10	
§  Many	other	effects	are	not	included.	
32
Conclusion	
§  Heat	transfer	enhancement	using	nanoaerosol	has	been	experimentally	
demonstrated	for	the	first	/me.	
§  Large	heat	transfer	enhancement	(~36%)	was	observed	at	rela/vely	low	par/cle	
loading	(~0.35%).	
§  Experimental	data	is	proved	to	be	sta/s/cally	significant.	
§  Observed	trends	are	consistent	with	theory	proposed	by	Murray.	
§  Murray’s	model	is	modified	for	free-molecular	and	transi/on	regime.	
—  Transi/on	model	agrees	with	experimental	data.	
—  Transi/on	model	extended	to	predict	effect	of	par/cle	size	over	mass	loading	
0.25%	-	1%.	
—  Other	effects	need	to	be	incorporated.		
33
Acknowledgements	
§  Alberta	Innovates	Technology	Futures	
§  Natural	Sciences	and	Engineering	Research	Council	
§  Space	Engine	Systems		
§  University	of	Calgary	
§  Dr.	Craig	Johansen	
34
References	
1.  Maxwell,	J.	C.	(1881).	A	trea;se	on	electricity	and	magne;sm	(Vol.	1).	Clarendon	press.	
2.  Choi,	S.	U.	S.	(1995).	Enhancing	thermal	conduc/vity	of	fluids	with	nanopar/cles.	ASME-
Publica;ons-Fed,	231,	99-106.		
3.  Zeinali	Heris,	S.,	Etemad,	S.	G.,	&	Nasr	Esfahany,	M.	(2006).	Experimental	inves/ga/on	
of	oxide	nanofluids	laminar	flow	convec/ve	heat	transfer.Interna;onal	Communica;ons	
in	Heat	and	Mass	Transfer,	33(4),	529-535.		
4.  Xuan,	Y.,	&	Li,	Q.	(2003).	Inves/ga/on	on	convec/ve	heat	transfer	and	flow	features	of	
nanofluids.	Journal	of	Heat	transfer,	125(1),	151-155	
5.  Murray,	D.	B.	(1994).	Local	enhancement	of	heat	transfer	in	a	par/culate	cross	flow—I	
Heat	transfer	mechanisms.	Interna;onal	journal	of	mul;phase	flow,	20(3),	493-504.	
6.  Murray,	D.	B.	(1994).	Local	enhancement	of	heat	transfer	in	a	par/culate	cross	flow—II	
Experimental	data	and	predicted	trends.	Interna;onal	journal	of	mul;phase	flow,	20(3),	
505-513.	
7.  Bianco,	V.,	Manca,	O.,	Nardini,	S.,	and	Vafai,	K.,	Heat	Transfer	Enhancement	With	
Nanouids,	April	1	2015,	CRC	Press	
35

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Enhancement of Convective Heat Transfer Using Aluminum Oxide Nanoaerosol