Boundary layer measurements on an airfoil at low Reynolds numbers inan accelerating flow from a nonzero base velocity
27th Aerospace Sciences Meeting ; 1989 ; Reno , NV , U.S.A.
01.01.1989
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Airfoil Boundary Layer and Wake Development at Low Reynolds Numbers
British Library Conference Proceedings | 2005
|Boundary Layer and Near-Wake Measurements of NACA 0012 Airfoil at Low Reynolds Numbers
British Library Conference Proceedings | 2009
|