Orbiter Gap Filler Bending Model for Re-Entry-Reference-Cited by-同舟云学术

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Orbiter Gap Filler Bending Model for Re-Entry

Published:2007-01-08 Issue: Volume: Page:
ISSN:
Container-title:45th AIAA Aerospace Sciences Meeting and Exhibit
language:
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Author:

Campbell Charles¹,Driver David²,Alter Stephen³,Fasanella Edwin³,Wood William³,Stone Jeffrey⁴

Affiliation:

1. NASA Johnson Space Center

2. NASA Ames Research Center

3. NASA Langley Research Center

4. The Boeing Company

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2007-413

Reference21 articles.

1. Shuttle Orbiter Experimental Boundary-Layer Transition Results with Isolated Roughness

2. Isolated roughness induced boundary-layer transition - Shuttle Orbiter ground tests and flight experience

3. Bertin,J.J.,andStetson,K.F."TheEffectofSurfaceRoughnessonShuttleOrbiterBoundary-LayerTransition,"Technical Report JSC-27358, NASA Johnson Space Center, January 1996.

Cited by 4 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Thermal Response of Supersonic Airflow to a Fin Protrusion Situated on a Curved Surface;Journal of Heat Transfer;2009-08-26

2. Discrete-Roughness Transition for Hypersonic Flight Vehicles;Journal of Spacecraft and Rockets;2008-03

3. Orbiter Entry Boundary Layer Flight Testing;46th AIAA Aerospace Sciences Meeting and Exhibit;2008-01-07

4. Rapid Aerothermal Simulations of Damage and Repair During a Space Shuttle Mission;48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference;2007-04-23

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