Influence of flowfield and vehicle parameters on engineering aerothermal methods
- 12 June 1989
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 9 references indexed in Scilit:
- Application of axisymmetric analog for calculating heating in three-dimensional flowsJournal of Spacecraft and Rockets, 1987
- Engineering flowfield method with angle-of-attack applicationsJournal of Spacecraft and Rockets, 1985
- Hypersonic Three-Dimensional Viscous Shock-Layer Flows over Blunt BodiesAIAA Journal, 1978
- Aerodynamic Heating on 3-D Bodies Includingthe Effects of Entropy-Layer SwallowingJournal of Spacecraft and Rockets, 1975
- 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
- An Investigation of Laminar, Transitional, and Turbulent Heat Transfer on Blunt-Nosed Bodies in Hypersonic FlowJournal of the Aerospace Sciences, 1960
- Laminar Heat Transfer Around Blunt Bodies in Dissociated AirJournal of the Aerospace Sciences, 1959
- Theory of Stagnation Point Heat Transfer in Dissociated AirJournal of the Aerospace Sciences, 1958