Heat transfer effects in nano-aluminum combustion at high temperatures

被引:59
作者
Allen, David [1 ]
Krier, Herman [1 ]
Glumac, Nick [1 ]
机构
[1] Univ Illinois, Mech Sci & Engn Dept, Urbana, IL 61801 USA
关键词
Nano-aluminum combustion; Heat transfer; Shock tube; BURN TIME; PARTICLE; NANOALUMINUM; OXIDATION; PRESSURE;
D O I
10.1016/j.combustflame.2013.07.010
中图分类号
O414.1 [热力学];
学科分类号
摘要
Recent measurements of nano-aluminum combustion in which burning time and peak particle temperature are measured simultaneously have suggested that heat transfer models currently used for burning nanoparticles may significantly overestimate heat losses during combustion. By applying conventional non-continuum heat transfer correlations to burning nano-aluminum particles, the observed peak temperatures, which greatly exceed the ambient temperature, should only be observable if the burning time were very short, of the order of 1 mu s, whereas the observed burning time is two orders of magnitude larger. These observations can be reconciled if the energy accommodation coefficient for these conditions is of the order of 0.005, which is the value suggested by Altman, instead of approximately unity, which is the common assumption. Experimental data obtained in the heterogeneous shock tube under a wide array of conditions are compared with basic heat transfer models, and the agreement of both peak temperature values and emission intensity traces for low energy accommodation coefficients supports the hypothesis of Altman and co-workers. (C) 2013 The Combustion Institute. Published by Elsevier Inc. All rights reserved.
引用
收藏
页码:295 / 302
页数:8
相关论文
共 25 条
[1]  
Altman I. S., 1999, Journal of Physical Studies, V3, P456
[2]   Experimental estimate of energy accommodation coefficient at high temperatures [J].
Altman, IS ;
Lee, D ;
Song, J ;
Choi, M .
PHYSICAL REVIEW E, 2001, 64 (05) :4-052202
[3]  
[Anonymous], 1996, COMPUTER PROGRAM CAL
[4]   Oxidizer and pressure effects on the combustion of 10-μm aluminum particles [J].
Bazyn, T ;
Krier, H ;
Glumac, N .
JOURNAL OF PROPULSION AND POWER, 2005, 21 (04) :577-582
[5]   Combustion of nanoaluminum at elevated pressure and temperature behind reflected shock waves [J].
Bazyn, Tim ;
Krier, Herman ;
Glumac, Nick .
COMBUSTION AND FLAME, 2006, 145 (04) :703-713
[6]   Correlating aluminum burning times [J].
Beckstead, MW .
COMBUSTION EXPLOSION AND SHOCK WAVES, 2005, 41 (05) :533-546
[7]   1ST OBSERVATIONS ON BREAK-UP OF PARTICLE AGGLOMERATES IN SHOCK-WAVES [J].
BRANDT, O ;
RAJATHURAI, AM ;
ROTH, P .
EXPERIMENTS IN FLUIDS, 1987, 5 (02) :86-94
[8]  
Brown J., 2007, THESIS
[9]  
Forney L., 1983, PARTICUL SCI TECHNOL, V1, P419
[10]   Temperature measurements of aluminum particles burning in carbon dioxide [J].
Glumac, N ;
Krier, H ;
Bazyn, T ;
Eyer, R .
COMBUSTION SCIENCE AND TECHNOLOGY, 2005, 177 (03) :485-511