Erosive burning of a solid propellant in a supersonic flow

被引：1
作者：
Arkhipov, VA [1 ]
Zimin, DA [1 ]
机构：
[1] Tomsk State Univ, Inst Appl Math & Mech, Tomsk 634050, Russia
来源：
COMBUSTION EXPLOSION AND SHOCK WAVES | 1998年 / 34卷 / 01期
关键词：
Mach Number; Supersonic Flow; Solid Propellant; Critical Cross Section; Erosion Coefficient;
D O I：
10.1007/BF02671818
中图分类号：
O414.1 [热力学];
学科分类号：
摘要：
We present results of an experimental study of burning of a ballistite solid propellant (gun powder Ii) in a supersonic how. It is shown that the criterial dependence of the erosion coefficient on the Vilyunov parameter obtained on the basis of experimental results in a subsonic and a supersonic how describes satisfactorily experimental data for a supersonic flow in the examined range of Mach numbers M = 1-2.8 as well. A more correct approximation formula for the range of parameters considered is derived. The specific features of the how along the surface of a solid propellant at M > 1 is analyzed, and this analysis has revealed some problems in the interpretation of experimental data.
引用
收藏
页码：55 / 57
页数：3
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