Effect of porosity strength on passive shock-wave/boundary-layer control
- 1 May 1987
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 25 (5) , 757-758
- https://doi.org/10.2514/3.9693
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- Passive shockwave boundary layer control experiments on a circular arc modelPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1986
- 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