Partial contents include: (1) Shock Wave Boundary Layer Interactions in High Mach Number Flows: A Critical Survey of Current Numerical Prediction Capabilities; (2) Hypersonic Laminar-Turbulent Transition; (3) Real Gas / Blunt Cone Phase II Report; (4) Extrapolation from Wind Tunnel to Flight: Shuttle Orbiter Aerodynamics; (5) Real-Gas Aerothermodynamics Test Facilities.
Hypersonic Experimental and Computational Capability, Improvement and Validation. Volume 2. (l'Hypersonique experimentale et de calcul - capacite, ameliorafion et validation)
1998
172 pages
Report
Keine Angabe
Englisch
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