Computational Fluid Dynamics for Winged Re-entry Vehicles at Hypersonic Conditions
Author:
Affiliation:
1. NASA Ames Research Center
2. ELORET Corporation
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2004-2537
Reference52 articles.
1. Computational Aerothermodynamic Analysis for the STS-107 Accident Investigation
2. LAURA Aerothermodynamic Computations for Space Shuttle Columbia STS-107 Baseline and Damage Scenarios
3. Simulation of Flow Through Breach in Leading Edge at Mach 24
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3. Computational Analysis of Semi-Elliptical Nozzle Arc-Jet Experiments: Calibration Plate, Wing Leading Edge;AIAA Journal;2007-01
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