Effect of Transition on Three-Dimensional Shock- Wave/Boundary-Layer Interaction
- 1 March 1972
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 10 (3) , 361-363
- https://doi.org/10.2514/3.50097
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- Survey of viscous interactions associated with high Mach number flightAIAA Journal, 1971
- Strahlungsenergietransport mit Absorption in zylindrischen BögenThe European Physical Journal A, 1968
- An investigation of flow separation and aerodynamic controls at hypersonic speeds.Journal of Aircraft, 1966
- Continuum radiation from partially ionized argon.AIAA Journal, 1966