Computation of transonic flow around airfoils with trailing edge andshock/boundary layer interactions
- 1 June 1984
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 21 (6) , 380-388
- https://doi.org/10.2514/3.44976
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- Transonic shock/turbulent boundary-layer interaction on curved surfacesJournal of Aircraft, 1983
- Application of a Shock-Turbulent Boundary-Layer Interaction Theory in Transonic Flowfield AnalysisPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1982
- Airfoil Flow Analysis with a Special Solution for Shock/Boundary-Layer InteractionAIAA Journal, 1981