HIGH-FREQUENCY COMBUSTION INSTABILITY IN ROCKET MOTOR WITH CONCENTRATED COMBUSTION

被引：7

作者：

CROCCO, L

CHENG, SI

机构：

来源：

JOURNAL OF THE AMERICAN ROCKET SOCIETY | 1953年 / 23卷 / 05期

关键词：

D O I：

10.2514/8.4623

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：301 / &

共 8 条

[1] ASPECTS OF COMBUSTION STABILITY IN LIQUID PROPELLANT ROCKET MOTORS .1. FUNDAMENTALS - LOW FREQUENCY INSTABILITY WITH MONOPROPELLANTS
CROCCO, L
[J]. JOURNAL OF THE AMERICAN ROCKET SOCIETY, 1951, 21 (06): : 163 - 178
[2] CROCCO L, 1953, J AM ROCKET SOC, V22, P7
[3] CROCCO L, 1952, 8TH INT C APPL MATH
[4] CROCCO L, 1952, 4TH S COMB
[5] GUNDER DF, 1950, J APPL MECH-T ASME, V17, P327
[6] A THEORY OF UNSTABLE COMBUSTION IN LIQUID PROPELLANT ROCKET SYSTEMS
SUMMERFIELD, M
[J]. JOURNAL OF THE AMERICAN ROCKET SOCIETY, 1951, 21 (05): : 108 - 114
[7] THE TRANSFER FUNCTIONS OF ROCKET NOZZLES
TSIEN, HS
[J]. JOURNAL OF THE AMERICAN ROCKET SOCIETY, 1952, 22 (03): : 139 - &
[8] YACHTER M, 1951, J APPL MECH, V18, P114