Aluminum combustion in a solid rocket motor environment

被引:66
作者
King, Merrill K. [1 ]
机构
[1] Software & Engn Associates Inc, Carson City, NV 89701 USA
关键词
Metal combustion; Aluminum; Solid rocket motors; MODEL;
D O I
10.1016/j.proci.2008.06.006
中图分类号
O414.1 [热力学];
学科分类号
摘要
A model for prediction of particle radius and oxide cap size/shape versus time for an aluminum particle tracking a stream-tube through a solid rocket motor port has been developed. Following preliminary calculations leading to it postulated flame structure, a quasi-steady model to predict instantaneous consumption of aluminum and generation of condensed oxide (both as a cap oil the aluminum particle and as smoke) as a function of instantaneous particle size, ambient conditions, and cumulative amount of oxide in the cap was developed. Finally, this model was imbedded into a framework tracking evolution of particle size, oxide cap size, and ambient conditions, which change as the particle travels along a stream-tube consuming oxidizer and releasing heat. Qualitative agreement was found between predictions and limited observations. (C) 2009 The Combustion Institute. Published by Elsevier Inc. All rights reserved.
引用
收藏
页码:2107 / 2114
页数:8
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