Boundary-Layer Measurements in Hypersonic Flow
- 1 January 1956
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 23 (1), 35-42
- https://doi.org/10.2514/8.3498
Abstract
No abstract availableKeywords
This publication has 6 references indexed in Scilit:
- Measurements of Turbulent Friction on a Smooth Flat Plate in Supersonic FlowJournal of the Aeronautical Sciences, 1954
- The problem of the turbulent boundary layerZeitschrift für angewandte Mathematik und Physik, 1954
- Turbulent Boundary Layers in Adverse Pressure GradientsJournal of the Aeronautical Sciences, 1954
- Measurements of Turbulent Skin Friction on Cylinders in Axial Flow at Subsonic and Supersonic VelocitiesJournal of the Aeronautical Sciences, 1953
- The Supersaturation of Nitrogen in a Hypersonic Wind TunnelJournal of Applied Physics, 1952
- Hypersonic Flow at a Mach Number of 10Journal of Applied Physics, 1951