The Effect of Controlled Three-Dimensional Roughness on Boundary-Layer Transition at Supersonic Speeds
- 1 April 1960
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aerospace Sciences
- Vol. 27 (4) , 261-271
- https://doi.org/10.2514/8.8501
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- Experiments on Boundary-Layer Transition at Supersonic SpeedsJournal of the Aeronautical Sciences, 1957
- Stress Analysis of Sheet-Stringer Panels with CutoutsJournal of the Aeronautical Sciences, 1953