An investigation of flow separation and aerodynamic controls at hypersonic speeds.
- 1 November 1966
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 3 (6) , 555-561
- https://doi.org/10.2514/3.43776
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- Mach 8 to 22 studies of flow separations due to deflected control surfacesAIAA Journal, 1964
- General Theory of High Speed AerodynamicsPublished by Walter de Gruyter GmbH ,1954