The effects of cooling on relaminarization
- 29 June 1987
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
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- Wind Tunnel Experiments Relating to Supersonic and Hypersonic Boundary-Layer TransitionAIAA Journal, 1975
- Reversion of turbulent to laminar flowJournal of Fluid Mechanics, 1968
- Laminarization of the Turbulent Boundary Layer in a Severe AccelerationJournal of Applied Mechanics, 1964
- The Smallest Height of Roughness Capable of Affecting Boundary-Layer TransitionJournal of the Aerospace Sciences, 1959
- Calculation of the Stability of the Laminar Boundary Layer in a Compressible Fluid on a Flat Plate with Heat TransferJournal of the Aeronautical Sciences, 1952