AN INTERPRETATION OF L COMBUSTION INSTABILITY IN TERMS OF ACOUSTIC INSTABILITY THEORY

被引:10
作者
COATES, RL
COHEN, NS
HARVILL, LR
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关键词
D O I
10.2514/3.4143
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
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页码:1097 / &
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共 18 条
[1]  
AKIBA R, 1959, 1ST P S INT ROCK AST, P74
[2]  
ANDERSON FA, 1963, AIAA J, V1, P2269
[3]  
ANDERSON FA, 1963, ICRPG19 SOL PROP C B, V3, P157
[4]  
ANDERSON FA, 1963, LOW PRESSURE COMBUST, V5, P13
[5]   NONACOUSTIC INSTABILITY OF COMPOSITE PROPELLANT COMBUSTION [J].
BECKSTEAD, MW ;
RYAN, NW ;
BAER, AD .
AIAA JOURNAL, 1966, 4 (09) :1622-+
[6]  
BECKSTEAD MW, 1966, 66111 AIAA
[7]  
BECKSTEAD MW, 1965, THESIS U UTAH SALT L
[8]   T-BURNER METHOD OF DETERMINING THE ACOUSTIC ADMITTANCE OF BURNING PROPELLANTS [J].
COATES, RL ;
HORTON, MD ;
RYAN, NW .
AIAA JOURNAL, 1964, 2 (06) :1119-1122
[9]  
COHEN NS, 1966, 2 P ICRPG COMB C SIL, V1, P677
[10]   A SIMPLIFIED MODEL OF UNSTABLE BURNING IN SOLID PROPELLANTS [J].
DENISON, MR ;
BAUM, E .
ARS JOURNAL, 1961, 31 (08) :1112-1122