On Strong Interaction for the Hypersonic Boundary Layer on an Inclined Wedge
- 1 November 1953
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 20 (11), 796
- https://doi.org/10.2514/8.2851
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- A Note on Hypersonic Viscous Flow over a Flat PlateJournal of the Aeronautical Sciences, 1953
- Shock-Wave Effects on the Laminar Skin Friction of an Insulated Flat Plate at Hypersonic SpeedsJournal of the Aeronautical Sciences, 1953
- On the Boundary-Layer Equations in Hypersonic Flow and Their Approximate SolutionsJournal of the Aeronautical Sciences, 1953
- Surface-Pressure Gradient and Shock-Front Curvature at the Edge of a Plane Ogive with Attached Shock FrontJournal of the Aeronautical Sciences, 1948