The study of the effect of the cavity on the flow over NACA 0012 and Selig 7003 aerofoil at Low Reynolds number using Vortex Shading Method
AIAA Scitech 2020 Forum
01.01.2020
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Low-Reynolds-Number Aerodynamic Performances of the NACA 0012 and Selig-Donovan 7003 Airfoils
Online Contents | 2013
|Aeroacoustic Study on a NACA 0012 Aerofoil
British Library Conference Proceedings | 1997
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AIAA | 1997
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