EXPERIMENTALLY DETERMINED ROCKET-EXHAUST FLOWFIELD IN A CONSTRICTIVE TUBE LAUNCHER

被引：5

作者：

BERTIN, JJ

BATSON, JL

机构：

[1] USA,MISSILE COMMAND,MISSILE RES DEV & ENGN LAB,HUNTSVILLE,AL

[2] UNIV TEXAS,DEPT AEROSP ENGN & ENGN MECH,AUSTIN,TX 78712

来源：

JOURNAL OF SPACECRAFT AND ROCKETS | 1975年 / 12卷 / 12期

关键词：

D O I：

10.2514/3.27869

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：711 / 717

页数：7

共 12 条

[1] FLOWFIELD PRODUCED BY ROCKET EXHAUST IMPINGEMENT OF A MULTITUBE LAUNCHER
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[4] PHOTOGRAPHIC TECHNIQUE FOR MEASURING TEMPERATURES IN LUMINOUS ROCKET-EXHAUST FLAMES
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[5] SECONDARY FLOWS IN A ROCKET LAUNCHER TUBE
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[J]. JOURNAL OF SPACECRAFT AND ROCKETS, 1981, 18 (02) : 119 - 126
[6] SCATTERING FROM A TURBULENT ROCKET-EXHAUST JET ILLUMINATED BY A FOCUED MICROWAVE BEAM
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[J]. ELECTRONICS LETTERS, 1971, 7 (19) : 597 - &
[7] VARIATIONS IN EDDY-CONVECTION SPEEDS IN ROCKET-EXHAUST FLOWS AND THEIR INFLUENCE ON RADIATED NOISE
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[J]. JOURNAL OF THE ACOUSTICAL SOCIETY OF AMERICA, 1963, 35 (11): : 1913 - &
[8] ROCKET EXHAUST FLOW IN TUBE LAUNCHERS
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[J]. JOURNAL OF SPACECRAFT AND ROCKETS, 1974, 11 (11) : 739 - 740
[9] INNER TUBE SLASHES COSTS OF ROCKET LAUNCHER TRAINING
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[J]. DESIGN NEWS, 1976, 31 (15) : 33 - 33
[10] Design and Analysis of Artillery Rocket Launcher Tube Mounted on Truck
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Nagarkar, Ish N.
Kulkarni, Nishad C.
Khadke, Satyajeet S.
[J]. International Journal of Vehicle Structures and Systems, 2022, 14 (03) : 401 - 406

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