Ice shapes and the resulting drag increase for a NACA 0012 airfoil
22nd Aerospace Sciences Meeting ; 1984 ; Reno , NV , U.S.A.
01.01.1984
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Viscous Drag Reduction Using Riblets on NACA 0012 Airfoil to Moderate Incidence
Online Contents | 1996
|Numerical Simulation of a Pitching NACA 0012 Airfoil
British Library Conference Proceedings | 2000
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