External Computational Aerothermodynamic Anaysis of the Space Shuttle Orbiter at STS-107 Flight Conditions

Author:

Reuther James1,McDaniel Ryan1,Brown James1,Prabhu Dinesh2,Saunders David2,Palmer Grant3

Affiliation:

1. NASA Ames Research Center

2. ELORET Corporation

3. ELLORET Corporation

Publisher

American Institute of Aeronautics and Astronautics

Cited by 5 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. 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

2. Assessment of Turbulent Shock-Boundary Layer Interaction Computations Using the OVERFLOW Code;45th AIAA Aerospace Sciences Meeting and Exhibit;2007-01-08

3. An Approach to Shock Envelope Grid Tailoring and Its Effect on Reentry Vehicle Solutions;45th AIAA Aerospace Sciences Meeting and Exhibit;2007-01-08

4. Pressure Gradient Effects on Hypersonic Cavity Flow Heating;44th AIAA Aerospace Sciences Meeting and Exhibit;2006-01-09

5. Computational Fluid Dynamics for Winged Re-entry Vehicles at Hypersonic Conditions;34th AIAA Fluid Dynamics Conference and Exhibit;2004-06-19

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