Boundary-Layer Interaction on a Yawed Infinite Wing in Hypersonic Flow
- 1 December 1959
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aerospace Sciences
- Vol. 26 (12) , 839-841
- https://doi.org/10.2514/8.8340
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- Turbulent Boundary Layers in Adverse Pressure GradientsJournal of the Aeronautical Sciences, 1954
- Generalized Theory of Convective Heat Transfer in a Free-Molecule FlowJournal of the Aeronautical Sciences, 1953