EFFECT OF MULTIDIMENSIONAL FLAMELETS IN COMPOSITE PROPELLANT COMBUSTION

被引:66
作者
PRICE, EW
机构
[1] Georgia Institute of Technology, Atlanta, GA
关键词
D O I
10.2514/3.23897
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
This article reviews the results of a series of studies involving two-dimensional models of combustion of solid propellants, The results presented are selected to illustrate the role of the kinetically limited leading-edge portion of the oxidizer/fuel ''diffusion'' flamelets in controlling burning rate and aluminum agglomeration. included are results from ''sandwich burning,'' gas burner, numerical modeling of the two-dimensional flame, and tests on propellants to validate the applicability to propellants.
引用
收藏
页码:717 / 728
页数:12
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