Fluid Dynamic Effects at Speeds From M = 11 to 15
- 1 February 1956
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 23 (2), 108-116
- https://doi.org/10.2514/8.3516
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- Hypersonic Viscous Flow over an Inclined WedgeJournal 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