Boundary-Layer Transition at Supersonic Speeds - Three-Dimensional Roughness Effects (Spheres)
- 1 August 1962
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aerospace Sciences
- Vol. 29 (8), 909-916
- https://doi.org/10.2514/8.9658
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- THE EFFECT OF DISTRIBUTED SURFACE ROUGHNESS ON LAMINAR FLOWPublished by Elsevier ,1961
- The Effect of Controlled Three-Dimensional Roughness on Boundary-Layer Transition at Supersonic SpeedsJournal of the Aerospace Sciences, 1960
- Transition Studies and Skin-Friction Measurements on an Insulated Flat Plate at a Mach Number of 5.8Journal of the Aeronautical Sciences, 1956
- Review of Published Data on the Effect of Roughness on Transition from Laminar to Turbulent FlowJournal of the Aeronautical Sciences, 1953