Turbulent heat transfer associated with control surface at Mach 6.
- 1 August 1968
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 6 (8) , 1612-1613
- https://doi.org/10.2514/3.4830
Abstract
No abstract availableThis publication has 1 reference indexed in Scilit:
- Boundary layer separation in hypersonic flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1966