STRESSES OWING TO INTERNAL PRESSURE IN SOLID PROPELLANT ROCKET GRAINS

被引：3

|

作者：

WILSON, HB

机构：

来源：

ARS JOURNAL | 1961年 / 31卷 / 03期

关键词：

D O I：

10.2514/8.5470

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

收藏

页码：309 / 317

页数：9

相关论文

共 50 条

[21] EFFECTS OF HIGH SPIN ON INTERNAL BALLISTICS OF A SOLID PROPELLANT ROCKET MOTOR
BRODDNER, S
ASTRONAUTICA ACTA, 1970, 15 (04): : 191 - &
[22] SOME STUDIES OF GRAVITATIONAL LOADS ON UNITED KINGDOM SOLID-PROPELLANT ROCKET GRAINS
HOPKINS, HG
LOCKETT, FJ
VERNON, JHC
JOURNAL OF SPACECRAFT AND ROCKETS, 1966, 3 (09) : 1415 - &
[23] A multilayered thick cylindrical shell under internal pressure and thermal loads applicable to solid propellant rocket motors
Renganathan, K
Rao, BN
Jana, MK
FORSCHUNG IM INGENIEURWESEN-ENGINEERING RESEARCH, 2000, 66 (02): : 57 - 66
[24] SOLID-PROPELLANT GRAINS
SEPPI, F
EXPERIMENTAL MECHANICS, 1967, 7 (04) : A37 - &
[25] STABILITY OF LONGITUDINAL OSCILLATIONS WITH PRESSURE AND VELOCITY COUPLING IN A SOLID PROPELLANT ROCKET
COATES, RL
COMBUSTION SCIENCE AND TECHNOLOGY, 1971, 3 (03) : 153 - &
[26] STABILITY OF LONGITUDINAL OSCILLATIONS WITH PRESSURE AND VELOCITY COUPLING IN A SOLID PROPELLANT ROCKET
CULICK, FEC
COMBUSTION SCIENCE AND TECHNOLOGY, 1970, 2 (04) : 179 - &
[27] PREDICTION OF INTERSTAGE PRESSURE IN MULTISTAGE SOLID-PROPELLANT ROCKET SYSTEMS
SMOOT, LD
AIAA JOURNAL, 1963, 1 (10) : 2361 - 2365
[28] The analysis method for the stability of rocket engine with solid propellant for low pressure
Chelaru, Teodor-Viorel
Coman, Adrian-Viorel
PROCEEDINGS OF THE 6TH IASME/WSEAS INTERNATIONAL CONFERENCE ON HEAT TRANSFER, THERMAL ENGINEERING AND ENVIRONMENT (HTE'08), PTS I AND II: NEW ASPECTS OF HEAT TRANSFER, THERMAL ENGINEERING AND ENVIRONMENT, 2008, : 322 - +
[29] INTERNAL BALLISTICS OF SLOTTED-TUBE SOLID-PROPELLANT ROCKET MOTORS
GLICK, RL
CAVENY, LH
THURMAN, JL
JOURNAL OF SPACECRAFT AND ROCKETS, 1967, 4 (04) : 525 - &
[30] Numerical simulation of chamber internal flowfield in spinning solid propellant rocket motor
Gao, Bo
Ye, Ding-you
Hou, Xiao
Guti Huojian Jishu/Journal of Solid Rocket Technology, 1999, 22 (02): : 8 - 11

← 1 2 3 4 5 →