Transition Studies and Skin-Friction Measurements on an Insulated Flat Plate at a Mach Number of 5.8
- 1 February 1956
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 23 (2) , 97-107
- https://doi.org/10.2514/8.3515
Abstract
No abstract availableThis publication has 7 references indexed in Scilit:
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- Measurements of Turbulent Friction on a Smooth Flat Plate in Supersonic FlowJournal of the Aeronautical Sciences, 1954
- Variation of Transition Reynolds Number with Mach NumberJournal of the Aeronautical Sciences, 1953
- Measurements of Turbulent Skin Friction on Cylinders in Axial Flow at Subsonic and Supersonic VelocitiesJournal of the Aeronautical Sciences, 1953
- The Compressible Boundary LayerJournal of the Aeronautical Sciences, 1952
- Two-Dimensional Jet Mixing of a Compressible FluidJournal of the Aeronautical Sciences, 1949
- Boundary Layer in Compressible FluidsJournal of the Aeronautical Sciences, 1938