EFFECT OF MULTIDIMENSIONAL FLAMELETS IN COMPOSITE PROPELLANT COMBUSTION

被引：27

作者：

LEE, ST ^{[1
]}

PRICE, EW ^{[1
]}

SIGMAN, RK ^{[1
]}

机构：

[1] GEORGIA INST TECHNOL,ATLANTA,GA 30332

来源：

JOURNAL OF PROPULSION AND POWER | 1994年 / 10卷 / 06期

关键词：

D O I：

10.2514/3.23813

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

Studies of edge burning of oxidizer-fuel laminae were extended by inclusion of different sizes of fine ammonium perchlorate (AP) into the binder lamina to study the combustion zone microstructure in composite-propellant combustion. Different modes of burning in heterogeneous systems resulting from pressure effects, AP particle-size effects, lamina thickness, and AP/binder mix ratios were determined. Results are interpreted in terms of the effects on name structure and multidimensional processes in the combustion zone.

引用

页码：761 / 768

页数：8

共 13 条

[1]

Beckstead MW., 1970, AIAA J, V8, P2200, DOI [10.2514/3.6087, DOI 10.2514/3.6087]

[2] REVIEW OF COMPOSITE PROPELLANT BURN RATE MODELING [J].