ASPECTS OF COMBUSTION STABILITY IN LIQUID PROPELLANT ROCKET MOTORS .1. FUNDAMENTALS - LOW FREQUENCY INSTABILITY WITH MONOPROPELLANTS

被引:253
作者
CROCCO, L
机构
来源
JOURNAL OF THE AMERICAN ROCKET SOCIETY | 1951年 / 21卷 / 06期
关键词
D O I
10.2514/8.4393
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
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页码:163 / 178
页数:16
相关论文
共 6 条
[1]  
GUNDER DF, 1950, J APPL MECH-T ASME, V17, P327
[2]  
MINORSKY N, 1942, J APPLIED MECHANICS, V9, P67
[3]  
RANDALL LN, 1951, ROCKET APPLICATIONS
[4]   A THEORY OF UNSTABLE COMBUSTION IN LIQUID PROPELLANT ROCKET SYSTEMS [J].
SUMMERFIELD, M .
JOURNAL OF THE AMERICAN ROCKET SOCIETY, 1951, 21 (05) :108-114
[5]  
TAIT BW, 1951, J AM ROCKET SOC, V21, P83
[6]  
YACHTER M, 1951, J APPL MECH, V18, P114