Approximate Heating Analysis for the Windward Symmetry Plane of Shuttle-like Bodies at Large Angle of Attack
- 1 January 1982
- book chapter
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 15 references indexed in Scilit:
- Viscous flow over arbitrary geometries at high angle of attackPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1980
- Numerical Computation of Space Shuttle Laminar Heating and Surface StreamlinesJournal of Spacecraft and Rockets, 1977
- Numerical Computations of Orbiter Flowfields and Laminar Heating RatesJournal of Spacecraft and Rockets, 1977
- 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
- Inviscid Surface Streamlines and Heat Transfer on Shuttle-Type ConfigurationsJournal of Spacecraft and Rockets, 1973
- Inviscid hypersonic flow past smooth symmetric bodiesAIAA Journal, 1964
- The drag of a compressible turbulent boundary layer on a smooth flat plate with and without heat transferJournal of Fluid Mechanics, 1964
- Turbulent Heat Transfer on Blunt-Nosed Bodies in Two-Dimensional and General Three-Dimensional Hypersonic FlowJournal of the Aerospace Sciences, 1960