Experimental investigation of subsonic turbulent separated boundary layers on an airfoil
- 1 January 1977
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 14 (1) , 51-55
- https://doi.org/10.2514/3.44573
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- Near-Wakes of Elliptic Cylinders in Subcritical FlowAIAA Journal, 1975
- Prediction of Turbulent Separated Boundary LayersAIAA Journal, 1974
- A Class of Airfoils Designed for High Lift in Incompressible FlowJournal of Aircraft, 1973
- Mathematical model for two-dimensional multi-component airfoils in viscous flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1972