Experimental observation of the flame structure of a bimodal ammonium perchlorate composite propellant using 5 kHz PLIF

被引:29
作者
Hedman, T. D. [1 ]
Cho, K. Y. [1 ]
Satija, A. [1 ]
Groven, L. J. [1 ]
Lucht, R. P. [1 ]
Son, S. F. [1 ]
机构
[1] Purdue Univ, Maurice J Zucrow Labs, Dept Mech Engn, W Lafayette, IN 47906 USA
关键词
Ammonium perchlorate; Hydroxyl-terminated polybutadiene; Planar laser induced fluorescence; Composite propellant; Ignition delay; Particle size; SURFACE-STRUCTURE; BURNING RATE;
D O I
10.1016/j.combustflame.2011.07.007
中图分类号
O414.1 [热力学];
学科分类号
摘要
The self deflagration of a bimodal ammonium perchlorate (AP) and hydroxyl-terminated polybutadiene (HTPB) propellant was studied using high speed (5 kHz) planar laser induced fluoresemce (PLIF) for the first time. The qualitative OH concentration was characterized near the surface. In addition to OH, it was found that the larger AP particles can be imaged as they fluoresce when exposed to laser radiation centered at 283.2 nm. Single AP particle ignition delay, lifetime, and flame height are determined as a function of particle diameter over a range from 100 to 500 mu m at 1 atm within the burning sample. High speed visible imaging was also completed to confirm the trends seen during PLIF experiments, although the fluoresced particles have much improved contrast. Ignition delay times and single particle burn times were compared with a model proposed by Shannon and Peterson. The measured final diffusion flame height above a regressing AP crystal was compared with an expression used by the Beckstead, Derr, and Price (BDP) model. It was found that the AP/HTPB propellant flame structure varies significantly with particle size, even at 1 atm. The models are found to adequately predict the observed trends, but do not capture the interaction of adjacent particles. The interaction of particles close to each other appear to affect behavior significantly and more detailed modeling is needed. It is shown that 5 kHz OH PLIF can be a valuable tool to characterize AP composite propellant combustion. (C) 2011 The Combustion Institute. Published by Elsevier Inc. All rights reserved.
引用
收藏
页码:427 / 437
页数:11
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