Effect of Airfoil Shape and Reynolds Number on Leading Edge Vortex Shedding in Unsteady Flows
30th AIAA Applied Aerodynamics Conference
01.01.2012
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Effect of Airfoil Shape and Reynolds Number on Leading Edge Vortex Shedding in Unsteady Flows
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