Engineering flowfields and heating rates for highly swept wing leading edges
- 1 September 1976
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 13 (9) , 540-546
- https://doi.org/10.2514/3.27926
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- Experimental Investigation of Supersonic Flow Past Double-Wedge ConfigurationsAIAA Journal, 1975
- High Velocity and Real-Gas Effects on Weak Two-Dimensional Shock-Interaction PatternsJournal of Spacecraft and Rockets, 1975
- Aerothermodynamic Aspects of Shock-Interference Patterns for Shuttle Configurations during EntryJournal of Spacecraft and Rockets, 1973
- Shock Interference Bell Aerospace, Heating in Hypersonic FlowsAIAA Journal, 1972
- Calculation of metric coefficients for streamline coordinates.AIAA Journal, 1972
- ANOMALOUS HEAT TRANSFER AND PRESSURE DISTRIBUTIONS ON BLUNT BODIES AT HYPERSONIC SPEEDS IN THE PRESENCE OF AN IMPINGING SHOCK.Published by Office of Scientific and Technical Information (OSTI) ,1968