Heat Transfer to Separated and Reattached Subsonic Turbulent Flows Obtained Downstream of a Surface Step
- 1 December 1959
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aerospace Sciences
- Vol. 26 (12), 809-814
- https://doi.org/10.2514/8.8324
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Velocity and Temperature Profiles in Turbulent Boundary Layers With Tangential InjectionJournal of Heat Transfer, 1962
- Experiments on two-dimensional flow over a normal wallJournal of Fluid Mechanics, 1956
- Heat Transfer to Turbulent Boundary Layers With Variable Free-Stream VelocityTransactions of the American Society of Mechanical Engineers, 1956