Passive shock wave/boundary layer control for transonic airfoil dragreduction
- 10 January 1983
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 3 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
- The Interaction Between Boundary Layer and Shock Waves in Transonic FlowJournal of the Aeronautical Sciences, 1946