Effects of modifications to the leading-edge region on the stalling characteristics of the NACA 63 1 -012 airfoil section
1950
22 S.
graph. Darst
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Book
English
Engineering Index Backfile | 1950
|Boundary-layer and stalling characteristics of NACA 64a010 airfoil section
Engineering Index Backfile | 1950
|Boundary-layer and stalling characteristics of NACA 64A006 airfoil section
Engineering Index Backfile | 1949
|