Airfoil Flow Analysis with a Special Solution for Shock/Boundary-Layer Interaction
- 1 December 1981
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 19 (12) , 1540-1546
- https://doi.org/10.2514/3.60092
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Theory of viscous transonic flow over airfoils at high Reynolds numberPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1977
- Analytical Theory of Transonic Normal Shock-Turbulent Boundary-Layer InteractionAIAA Journal, 1976
- Supercritical Wing Sections IIPublished by Springer Nature ,1975