An Engineering Inviscid-Reacting Boundary Layer Method for Calculation of Hypersonic Aerodynamic Heating
Author:
Affiliation:
1. Amirkabir Univ. of Technology
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2005-510
Reference17 articles.
1. Engineering aerodynamic heating method for hypersonic flow
2. Lawrence, S., L., Chaussee, S., L., and Tannehill C., J. "Application of an Upwind Algorithm to the Three-Dimensional Parabolized Navier-Stokes Equations,"AIAA87-1112, June1987.
3. Hypersonic Three-Dimensional Viscous Shock-Layer Flows over Blunt Bodies
4. Inviscid Surface Streamlines and Heat Transfer on Shuttle-Type Configurations
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