The Effect of Leading-Edge Bluntness on a Laminar Supersonic Boundary Layer
- 1 June 1954
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 21 (6) , 373-382
- https://doi.org/10.2514/8.3041
Abstract
No abstract availableKeywords
This publication has 1 reference indexed in Scilit:
- Temperature and Velocity Profiles in the Compressible Laminar Boundary Layer with Arbitrary Distribution of Surface TemperatureJournal of the Aeronautical Sciences, 1949