Approximate heating analysis for the windward-symmetry plane of Shuttle-like bodies at large angle of attack
- 23 June 1981
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 8 references indexed in Scilit:
- Viscous flow over arbitrary geometries at high angle of attackPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1980
- Numerical Computations of Orbiter Flowfields and Laminar Heating RatesJournal of Spacecraft and Rockets, 1977
- Leeward heat transfer experiments on the shuttle orbiter fuselageJournal of Spacecraft and Rockets, 1976
- Engineering flowfields and heating rates for highly swept wing leading edgesJournal of Spacecraft and Rockets, 1976
- Effects of Surface Temperature and Reynolds Number on Leeward Shuttle HeatingJournal of Spacecraft and Rockets, 1976
- Calculation of the flow on a blunted cone at high angle of attackPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1975
- An approximate inviscid radiating flow-field analysis for sphere-cone Venusian entry vehiclesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1974
- Inviscid Surface Streamlines and Heat Transfer on Shuttle-Type ConfigurationsJournal of Spacecraft and Rockets, 1973