Boundary-Layer Transition Measurements at Mach Numbers from 5.4 to 7.4
- 1 September 1960
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aerospace Sciences
- Vol. 27 (9) , 719-720
- https://doi.org/10.2514/8.8724
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- Transition Studies and Skin-Friction Measurements on an Insulated Flat Plate at a Mach Number of 5.8Journal of the Aeronautical Sciences, 1956
- Effects of Pressure Gradient on Stability and Skin Friction in Laminar Boundary Layers in Compressible FluidsJournal of the Aeronautical Sciences, 1951