T-BURNERS - EXPERIMENTS COMPARED WITH THEORY

被引：1

作者：

HORTON, MD ^{[1
]}

COATES, RL ^{[1
]}

机构：

[1] BRIGHAM YOUNG UNIV,PROVO,UT 84601

来源：

JOURNAL OF SPACECRAFT AND ROCKETS | 1974年 / 11卷 / 01期

关键词：

D O I：

10.2514/3.62003

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：48 / 51

页数：4

共 10 条

[1] INTERACTION BETWEEN SOUND + FLOW IN ACOUSTIC CAVITIES - MASS MOMENTUM + ENERGY CONSIDERATIONS [J].

CANTRELL, RH ;

HART, RW .

JOURNAL OF THE ACOUSTICAL SOCIETY OF AMERICA, 1964, 36 (04) :697-&

[2] T-BURNER METHOD OF DETERMINING THE ACOUSTIC ADMITTANCE OF BURNING PROPELLANTS [J].

COATES, RL ;

HORTON, MD ;

RYAN, NW .

AIAA JOURNAL, 1964, 2 (06) :1119-1122

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

COATES, RL .

COMBUSTION SCIENCE AND TECHNOLOGY, 1971, 3 (03) :153-&

[4]

COATES RM, TO BE PUBLISHED

[5]

CULICK FEC, 1971, COMBUSTION SCIENCE T, V3, P153

[6]

CULICK FEC, 1972, TP5349 NAV WEAP CTR

[7] NONLINEAR EFFECTS IN INSTABILITY OF SOLID-PROPELLANT ROCKET MOTORS [J].

HART, RW ;

BIRD, JF ;

CANTRELL, RH ;

MCCLURES, FT .

AIAA JOURNAL, 1964, 2 (07) :1270-1273

[8]

HART RW, 1965, 10 S INT COMB, P1047

[9]

HORTON MD, 1963, 9 S INT COMB, P303

[10]

PRICE EW, 1961, COMBUST FLAME, V5, P149

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