Heat transfer characteristics of hypersonic waveriders with an emphasis on leading edge effects
- 6 July 1992
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- Transition in the Infinite Swept Attachment Line Boundary LayerAeronautical Quarterly, 1979
- Ballistics Range Boundary-Layer Transition Measurements on Cones at Hypersonic SpeedsPublished by Springer Nature ,1969