The effects of camber on the variation with Mach number of the aerodynamic characteristics of a 10-percent-thick modified NACA four-digit-series airfoil section
1953
34 S
graph. Darst
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Book
English