IGNITION OF SOLID-PROPELLANT CRACK TIP UNDER RAPID PRESSURIZATION

被引：11

作者：

KUMAR, M

KUO, KK

机构：

来源：

AIAA JOURNAL | 1980年 / 18卷 / 07期

关键词：

D O I：

10.2514/3.50824

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：825 / 833

页数：9

共 17 条

[1]

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[5]

HERMANCE CE, 1966, ASTRONAUT ACTA, V12, P95

[6] GAS PHASE IGNITION THEORY FOR HOMOGENEOUS PROPELLANTS UNDER SHOCK TUBE CONDITIONS [J].

HERMANCE, CE ;

KUMAR, RK .

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[7] IGNITION OF AN EVAPORATING FUEL IN A HOT STAGNANT GAS CONTAINING AN OXIDIZER [J].

HERMANCE, CE ;

SHINNAR, R ;

SUMMERFI.M .

AIAA JOURNAL, 1965, 3 (09) :1584-&

[8] IGNITION OF HOMOGENEOUS SOLID PROPELLANTS UNDER SHOCK TUBE CONDITIONS - FURTHER THEORETICAL DEVELOPMENT [J].

KUMAR, RK ;

HERMANCE, CE .

AIAA JOURNAL, 1971, 9 (08) :1615-&

[9]

KUMAR RK, 1972, COMBUST SCI TECHNOL, V4, P191

[10] CONVECTIVE BURNING IN SOLID-PROPELLANT CRACKS [J].

KUO, KK ;

CHEN, AT ;

DAVIS, TR .

AIAA JOURNAL, 1978, 16 (06) :600-607

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