Aerodynamic characteristics, database development, and flight simulation of the X-34 vehicle

被引：0

作者：

Pamadi, B.N. ^{[1
]}

Brauckmann, G.J. ^{[1
]}

Ruth, M.J. ^{[1
]}

Fuhrmann, H.D. ^{[1
]}

机构：

[1] NASA Langley Research Center, Hampton, VA 23681, United States

来源：

| 2001年 / American Inst. Aeronautics and Astronautics Inc.卷 / 38期

关键词：

Computer simulation - Database systems - Hypersonic aerodynamics - Subsonic aerodynamics - Trajectories - Unmanned vehicles - Wind tunnels;

D O I：

暂无

中图分类号：

学科分类号：

摘要：

An overview of the aerodynamic characteristics, development of the preflight aerodynamic database, and flight simulation of the NASA/Orbital X-34 vehicle is presented. To develop the aerodynamic database, wind-tunnel tests from subsonic to hypersonic Mach numbers, including ground-effect tests at low subsonic speeds, were conducted in various facilities at the NASA Langley Research Center. Where wind-tunnel test data were not available, engineering level analysis was used to fill the gaps in the database. Using these aerodynamic data, simulations have been performed for typical design reference missions of the X-34 vehicle.

引用

共 50 条

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Pamadi, BN
Brauckmann, GJ
Ruth, MJ
Fuhrmann, HD
JOURNAL OF SPACECRAFT AND ROCKETS, 2001, 38 (03) : 334 - 344
[2] X-34 vehicle aerodynamic characteristics
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JOURNAL OF SPACECRAFT AND ROCKETS, 1999, 36 (02) : 229 - 239
[3] NASA revamps X-34 testing, adds third flight vehicle
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AVIATION WEEK & SPACE TECHNOLOGY, 1999, 151 (09): : 28 - 28
[4] X-34 launch vehicle - Initial development issues
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Austin, T
French, D
Harris, G
Wrobel, W
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SPACE TECHNOLOGY AND APPLICATIONS INTERNATIONAL FORUM (STAIF-96), PTS 1-3: 1ST CONFERENCE ON COMMERCIAL DEVELOPMENT OF SPACE; 1ST CONFERENCE ON NEXT GENERATION LAUNCH SYSTEMS; 2ND SPACECRAFT THERMAL CONTROL SYMPOSIUM; 13TH SYMPOSIUM ON SPACE NUCLEAR POWER AND PROPULSION - FUTURE SPACE AND EARTH SCIENCE MISSIONS - SPECIAL TOPIC; REMOTE SENSING FOR COMMERCIAL, CIVIL AND SCIENCE APPLICATIONS - SPECIAL TOPIC, 1996, (361): : 539 - 544
[5] Aeroelastic analysis of the X-34 launch vehicle
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Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, 1999, 2 : 1321 - 1331
[6] Modeling and correlation of the X-34 launch vehicle
Blelloch, P
Blades, E
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[7] Modeling and correlation of the X-34 launch vehicle
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IMAC-XVIII: A CONFERENCE ON STRUCTURAL DYNAMICS, VOLS 1 AND 2, PROCEEDINGS, 2000, 4062 : 1276 - 1280
[8] Modeling and correlation of the X-34 launch vehicle
Blelloch, Paul A., 2000, SEM, United States (02):
[9] Powered flight of X-34 slipped to late fall
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AVIATION WEEK & SPACE TECHNOLOGY, 2000, 152 (05): : 36 - 36
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SOUND AND VIBRATION, 2000, 34 (03): : 18 - 24

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