RADIATIVE IGNITION OF DOUBLE BASE PROPELLANTS .2. PRE-IGNITION EVENTS AND SOURCE EFFECTS

被引：33

作者：

DELUCA, L ^{[1
]}

OHLEMILLER, TJ ^{[1
]}

CAVENY, LH ^{[1
]}

SUMMERFIELD, M ^{[1
]}

机构：

[1] PURDUE UNIV,W LAFAYETTE,IN 47907

来源：

AIAA JOURNAL | 1976年 / 14卷 / 08期

关键词：

D O I：

10.2514/3.7193

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：1111 / 1117

页数：7

共 18 条

[1] AN APPROXIMATE BUT COMPLETE MODEL FOR IGNITION RESPONSE OF SOLID PROPELLANTS [J].

BAER, AD ;

RYAN, NW .

AIAA JOURNAL, 1968, 6 (05) :872-&

[2]

BASTRESS EK, 1964, AF046119065 CONTR

[3]

BASTRESS EK, 1966, 2ND P ICPRG COMB C, P551

[4]

BEYER RB, 1960, SOLID PROPELLANT ROC, V1, P674

[5] INFLUENCE OF THERMAL-RADIATION ON SOLID-PROPELLANT BURNING RATE [J].

CAVENY, LH ;

OHLEMILLER, TJ ;

SUMMERFIELD, M .

AIAA JOURNAL, 1975, 13 (02) :202-205

[6]

CAVENY LH, 1975, 13TH AIAA AER SCI M

[7]

CAVENY LH, TO BE PUBLISHED

[8] RADIATIVE IGNITION OF DOUBLE BASE PROPELLANTS .2. PRE-IGNITION EVENTS AND SOURCE EFFECTS [J].

DELUCA, L ;

OHLEMILLER, TJ ;

CAVENY, LH ;

SUMMERFIELD, M .

AIAA JOURNAL, 1976, 14 (08) :1111-1117

[9]

DELUCA L, IN PRESS

[10]

KONDRIKOV BN, 1970, 13TH INT S COMB

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