Comparison of viscous shock layer and boundary layer reentry heatingtechniques for Orbiter nose cap
Author:
Affiliation:
1. NASA, Johnson Space Center, Houston, TX
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1986-1350
Reference35 articles.
1. Lee,D. B.andHarthun,M.€I."AerothermodynamieEntry Environment ofthe SpaceShuttleOrbiter."Entrv Vehicle HeatingandThermal ProtectionSystems: SpaceShuttle, SolarStarprobe.Jupiter GalileoProbe,Vol.85of& PropressinAstronautics and Aeronautics, 1983,pp. 3-20.
2. Hypersonic Three-Dimensional Viscous Shock-Layer Flows over Blunt Bodies
3. Comparative analysis of numerical schemes for hypersonic re-entry flows
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