Comparison of nonequilibrium viscous-shock-layer solutions with shuttle heating measurement
- 1 April 1990
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Thermophysics and Heat Transfer
- Vol. 4 (2) , 162-169
- https://doi.org/10.2514/3.159
Abstract
No abstract availableKeywords
This publication has 13 references indexed in Scilit:
- Three-dimensional effects upon real gas flows past the Space ShuttlePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1984
- Chemical equilibrium laminar or turbulent three-dimensional viscous shock-layer flowsJournal of Spacecraft and Rockets, 1983
- Effects of nonequilibrium and surface catalysis on Shuttle heat transfer - A reviewPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1983
- Analysis of STS-2 experimental heating rates and transition dataJournal of Spacecraft and Rockets, 1983
- Benchmark determination of Shuttle Orbiter entry aerodynamic heat-transfer dataJournal of Spacecraft and Rockets, 1983
- Viscous-shock-layer heating analysis for the shuttle windward-symmetry plane with surface finite catalytic recombination ratesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1982
- Viscous shock-layer predictions for hypersonic laminar or turbulent flows in chemical equilibrium over the windward surface of a Shuttle-like vehiclePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1982
- Hypersonic Three-Dimensional Viscous Shock-Layer Flows over Blunt BodiesAIAA Journal, 1978
- Numerical Computation of Space Shuttle Laminar Heating and Surface StreamlinesJournal of Spacecraft and Rockets, 1977
- Approximate Formula for the Thermal Conductivity of Gas MixturesPhysics of Fluids, 1958