On "Transformation of the Compressible Turbulent Boundary Layer"
- 1 August 1959
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aerospace Sciences
- Vol. 26 (8), 528-529
- https://doi.org/10.2514/8.8175
Abstract
No abstract availableKeywords
This publication has 3 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
- The law of the wall in turbulent shear flowPublished by Springer Nature ,1955
- Measurements of Turbulent Friction on a Smooth Flat Plate in Supersonic FlowJournal of the Aeronautical Sciences, 1954