Passive shock-wave/boundary-layer control on a wall-mounted model
- 1 February 1987
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 25 (2) , 275-278
- https://doi.org/10.2514/3.9618
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- Supercritical airfoil drag reduction by passive shock wave/boundary layer control in the Mach number range .75 to .90Published by American Institute of Aeronautics and Astronautics (AIAA) ,1985
- Porous Airfoils in Transonic FlowAIAA Journal, 1984
- Effects of local boundary layer suction on shock-boundary layer interaction and shock-induced separationPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1984