Comparison between dynamic stability boundaries for NPL 9615 and NACA 0012 aerofoils pitching about the quarter-chord
1974
29 S., [12] Bl.
graph. Darst.
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Book
English
NPL 9615 and NACA 0012 - a comparison of aerodynamic data
TIBKAT | 1973
|Numerical Simulation of a Pitching NACA 0012 Airfoil
British Library Conference Proceedings | 2000
|Leading-Edge Flow Structure of a Dynamically Pitching NACA 0012 Airfoil
Online Contents | 2013
|