Measurements in a separation bubble on an airfoil using laser velocimetry
- 1 April 1990
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 28 (4) , 584-592
- https://doi.org/10.2514/3.10433
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- Low-Reynolds-number airfoil design for the M.I.T. Daedalus prototype- A case studyJournal of Aircraft, 1988
- Boundary-layer measurements on an airfoil at low Reynolds numbersJournal of Aircraft, 1988
- A study of the laminar separation bubble on an airfoil at low Reynolds numbers using flow visualization techniquesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Experimental determination of the laminar separation bubble characteristics on an airfoil at low Reynolds numbersPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1986
- Prediction of Incompressible Separated Boundary Layers Including Viscous-Inviscid InteractionJournal of Fluids Engineering, 1979
- Further solutions of the Falkner-Skan equationMathematical Proceedings of the Cambridge Philosophical Society, 1954