PULSING TECHNIQUES FOR SOLID-PROPELLANT ROCKET MOTORS - MODELING AND COLD-FLOW TESTING

被引：10

作者：

BAUM, JD

LOVINE, RL

LEVINE, JN

机构：

[1] UNIV DAYTON,RES INST,DAYTON,OH 45469

[2] AEROJET TACT SYST,SACRAMENTO,CA

来源：

JOURNAL OF SPACECRAFT AND ROCKETS | 1983年 / 20卷 / 02期

关键词：

D O I：

10.2514/3.28372

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：150 / 157

页数：8

共 16 条

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LEVINE, JN .

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[2] NONLINEAR AXIAL COMBUSTION INSTABILITY IN SOLID PROPELLANT MOTORS [J].

BROWNLEE, WG .

AIAA JOURNAL, 1964, 2 (02) :275-284

[3]

COMBS LP, 1968, AFRPLTR68018

[4]

DICKINSON LA, 1962, ARSJ-AM ROCKET SOC J, V32, P643

[5] SELF-ADJUSTING HYBRID SCHEMES FOR SHOCK COMPUTATIONS [J].

HARTEN, A ;

ZWAS, G .

JOURNAL OF COMPUTATIONAL PHYSICS, 1972, 9 (03) :568-&

[6]

HARTEN A, 1977, AFOSR TR770659, V3

[7] SYSTEMS OF CONSERVATION LAWS [J].

LAX, P ;

WENDROFF, B .

COMMUNICATIONS ON PURE AND APPLIED MATHEMATICS, 1960, 13 (02) :217-237

[8]

LEVINE JN, 1974, AFRPL TR7445

[9]

LEVINE JN, 1981, AIAA811524 PAP

[10]

LOVINE RL, 1981, 18TH JANNAF COMB M P

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