Experimental Investigation of Turbulent Boundary Layers in Hypersonic Flow
- 1 January 1955
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 22 (1) , 1-9
- https://doi.org/10.2514/8.3262
Abstract
No abstract availableKeywords
This publication has 6 references indexed in Scilit:
- Design and Calibration of Stagnation Temperature Probes for Use at High Supersonic Speeds and Elevated TemperaturesJournal of Applied Physics, 1954
- An Experimental Study of a Hypersonic Wind-Tunnel DiffuserJournal of the Aeronautical Sciences, 1953
- Summary of Recent Experimental Investigations in the N.O.L. Hyperballistics Wind TunnelJournal of the Aeronautical Sciences, 1951
- Turbulent Boundary-Layer Characteristics at Supersonic Speeds-Theory and ExperimentJournal of the Aeronautical Sciences, 1950
- On Some Series of Bessel FunctionsJournal of Mathematics and Physics, 1947
- Superaerodynamics, Mechanics of Rarefied GasesJournal of the Aeronautical Sciences, 1946