EFFECT OF COMPOSITIONAL VARIABLES UPON OSCILLATORY COMBUSTION OF SOLID ROCKET PROPELLANTS

被引：26

作者：

HORTON, MD

RICE, DW

机构：

来源：

关键词：

D O I：

10.1016/0010-2180(64)90053-7

中图分类号：

O414.1 [热力学];

学科分类号：

摘要：

引用

页码：21 / &

共 10 条

[1]

CARPENTER C, 1942, CITJDC13

GREEN, L .

JET PROPULSION, 1958, 28 (03) :159-164

HART, RW ;

MCCLURE, FT .

[4] AMPLIFICATION AND ATTENUATION OF SOUND BY BURNING PROPELLANTS [J].

HART, RW ;

CANTRELL, RH .

[5]

HORTON MD, NAVWEPS RESEARCH DEP

[6]

HORTON MD, 1963, 9 S INT COMB, P303

[7] INTERACTION BETWEEN SOUND AND FLOW - STABILITY OF T-BURNERS [J].

MCCLURE, FT ;

HART, RW ;

CANTRELL, RH .

[8]

PRICE EW, 1960, SOLID PROPELLANT ROC, P561

[9]

STRITTMATER R, 1963, 9TH S INT COMB, P311

[10]

SUMMERFIELD M, 1960, SOLID PROPELLANT ROC, P561