Numerical simulation of re-entry flow around the Space Shuttle with finite-rate chemistry
Author:
Affiliation:
1. National Aerospace Laboratory, Tokyo 182, Japan
2. University of Tokyo, Tokyo 113, Japan
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.46283
Reference29 articles.
1. Space Shuttle entry aerodynamic comparisons of flight 1 with preflight predictions
2. Hypersonic Mach number and real gas effects on Space Shuttle Orbiteraerodynamics
3. The versatility and reliability of Euler solvers based on high-accuracy TVD formulations
4. Approximate Riemann solvers, parameter vectors, and difference schemes
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