Porosity effect on supercritical airfoil drag reduction by shock wave/boundary layer control
- 25 June 1984
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- Passive shock wave/boundary layer control for transonic airfoil dragreductionPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1983
- Design of transonic airfoil sections using a similarity theoryPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1979