Laminar heat transfer to a two-dimensional backward facing step from the high-enthalpy supersonic flow in the shock tube
- 1 February 1964
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 2 (2) , 251-255
- https://doi.org/10.2514/3.2295
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- Some Experiments on Hypersonic Separated FlowsARS Journal, 1962
- Measurement of Turbulent Heat Transfer Rates on the Aft Portion and Blunt Base of a Hemisphere Cylinder in the Shock TubeJournal of Jet Propulsion, 1958