Heat transfer to wavy wall in hypersonic flow.
- 1 October 1967
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 5 (10), 1760-1767
- https://doi.org/10.2514/3.4301
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Mach 8 to 22 studies of flow separations due to deflected control surfacesAIAA Journal, 1964
- EFFECT OF SURFACE DISTORTIONS ON THE HEAT TRANSFER TO A WING AT HYPERSONIC SPEEDSAIAA Journal, 1963
- Recent Hypersonic Studies of Wings and BodiesARS Journal, 1961
- A Summary of Viscosity and Heat-Conduction Data for He, A, H2, O2, N2, CO, CO2, H2O, and AirTransactions of the American Society of Mechanical Engineers, 1951