An experimental investigation of heat transfer from a highly cooled turbulent boundary layer.
- 1 October 1968
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 6 (10) , 1912-1918
- https://doi.org/10.2514/3.4900
Abstract
No abstract availableKeywords
This publication has 7 references indexed in Scilit:
- Some effects of roughness and variable entropy on transition at a Mach number of 8Published by American Institute of Aeronautics and Astronautics (AIAA) ,1967
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- Boundary-Layer Transition on Blunt Bodies with Highly Cooled Boundary LayersJournal 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
- Engineering Relations for Heat Transfer and Friction in High-Velocity Laminar and Turbulent Boundary-Layer Flow Over Surfaces With Constant Pressure and TemperatureTransactions of the American Society of Mechanical Engineers, 1956
- Turbulent Boundary Layer in Compressible FluidsJournal of the Aeronautical Sciences, 1951