MODEL DESCRIBING EROSIVE COMBUSTION AND VELOCITY RESPONSE OF COMPOSITE PROPELLANTS

被引:37
作者
LENGELLE, G [1 ]
机构
[1] NATL OFF AEROSP STUDY & RES,ENERGETICS DEPT,CHATILLON,FRANCE
关键词
D O I
10.2514/3.49697
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
引用
收藏
页码:315 / 322
页数:8
相关论文
共 31 条
[1]  
BARRERE M, 1963, RECHERCHE AEROSP JUL, P25
[2]  
BASTRESS EK, 1961, ARS159761 PAP
[3]  
Beckstead M. W., 1971, 13TH S INT COMB PITT, P1047
[4]  
Beckstead MW., 1970, AIAA J, V8, P2200, DOI [10.2514/3.6087, DOI 10.2514/3.6087]
[5]   ROLE OF BINDERS IN SOLID-PROPELLANT COMBUSTION [J].
COHEN, NS ;
FLEMING, RW ;
DERR, RL .
AIAA JOURNAL, 1974, 12 (02) :212-218
[6]   A REVIEW OF CALCULATIONS FOR UNSTEADY BURNING OF A SOLID PROPELLANT [J].
CULICK, FEC .
AIAA JOURNAL, 1968, 6 (12) :2241-&
[7]  
CULICK FEC, 1967, ASTRONAUT ACTA, V13, P221
[8]   THE TURBULENT BOUNDARY LAYER ON CHEMICALLY ACTIVE ABLATING SURFACES [J].
DENISON, MR .
JOURNAL OF THE AEROSPACE SCIENCES, 1961, 28 (06) :471-479
[9]   A SIMPLIFIED MODEL OF UNSTABLE BURNING IN SOLID PROPELLANTS [J].
DENISON, MR ;
BAUM, E .
ARS JOURNAL, 1961, 31 (08) :1112-1122