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THEORY OF LIQUID PROPELLANT ROCKET COMBUSTION INSTABILITY AND ITS EXPERIMENTAL VERIFICATION

被引：26
作者：
CROCCO, L
GREY, J
HARRJE, DT
机构：
来源：
ARS JOURNAL | 1960年 / 30卷 / 02期
关键词：
D O I：
10.2514/8.5020
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：159 / 168
页数：10
相关论文
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BERMAN, K ;
CHENEY, SH .
JOURNAL OF THE AMERICAN ROCKET SOCIETY, 1953, 23 (02) :89-&
[2]   ASPECTS OF COMBUSTION STABILITY IN LIQUID PROPELLANT ROCKET MOTORS .2. LOW FREQUENCY INSTABILITY WITH BIPROPELLANTS - HIGH FREQUENCY INSTABILITY [J].
CROCCO, L .
JOURNAL OF THE AMERICAN ROCKET SOCIETY, 1952, 22 (01) :7-16
[3]   ASPECTS OF COMBUSTION STABILITY IN LIQUID PROPELLANT ROCKET MOTORS .1. FUNDAMENTALS - LOW FREQUENCY INSTABILITY WITH MONOPROPELLANTS [J].
CROCCO, L .
JOURNAL OF THE AMERICAN ROCKET SOCIETY, 1951, 21 (06) :163-178
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[5]  
CROCCO L, UNPUB SUBSTANTIATION
[6]  
Crocco L., 1956, AGARD MONOGRAPH, V8
[7]  
Crocco L, 1953, AEROTECHNICA, V33, P46
[8]  
GREY J, 1955, 216N PRINC U AER ENG
[9]  
GUNDER DF, 1950, J APPL MECH-T ASME, V17, P327
[10]  
LAMBIRIS S, 1947, PR75R PROJ SQUID TEC
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