COMBUSTION RESPONSE TO COMPOSITIONAL FLUCTUATIONS

被引：13

作者：

COHEN, NS ^{[1
]}

STRAND, LD ^{[1
]}

机构：

[1] CALTECH,JET PROP LAB,PASADENA,CA 91109

来源：

AIAA JOURNAL | 1985年 / 23卷 / 05期

关键词：

D O I：

10.2514/3.8981

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：760 / 767

页数：8

共 29 条

[1]

ANDREPONT WC, 1981, CPIA PUBL 347, V1, P1

[2] DETERMINATION OF SOLID-PROPELLANT ADMITTANCES BY THE IMPEDANCE TUBE METHOD [J].

BAUM, JD ;

DANIEL, BR ;

ZINN, BT .

AIAA JOURNAL, 1981, 19 (02) :214-220

[3]

BAUM JD, 1982, AIAA J, V20, P417, DOI 10.2514/3.51086

[4]

Beckstead MW., 1970, AIAA J, V8, P2200, DOI [10.2514/3.6087, DOI 10.2514/3.6087]

[5] REVIEW OF COMPOSITE PROPELLANT BURN RATE MODELING [J].

COHEN, NS .

AIAA JOURNAL, 1980, 18 (03) :277-293

[6] RESPONSE FUNCTION THEORIES THAT ACCOUNT FOR SIZE DISTRIBUTION EFFECTS - A REVIEW [J].

COHEN, NS .

AIAA JOURNAL, 1981, 19 (07) :907-912

[7] AN IMPROVED MODEL FOR THE COMBUSTION OF AP COMPOSITE PROPELLANTS [J].

COHEN, NS ;

STRAND, LD .

AIAA JOURNAL, 1982, 20 (12) :1739-1746

[8]

COHEN NS, 1981, CPIA PUBL 347, V3, P7

[9] A REVIEW OF CALCULATIONS FOR UNSTEADY BURNING OF A SOLID PROPELLANT [J].

CULICK, FEC .

AIAA JOURNAL, 1968, 6 (12) :2241-&

[10] STABILITY OF LONGITUDINAL OSCILLATIONS WITH PRESSURE AND VELOCITY COUPLING IN A SOLID PROPELLANT ROCKET [J].

CULICK, FEC .

COMBUSTION SCIENCE AND TECHNOLOGY, 1970, 2 (04) :179-&

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