Experimental investigation of an NACA 64A010 airfoil section with 41 suction slots on each surface for control of laminar boundary layer
1952
37 S
Ill., graph. Darst
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Book
English
Boundary-layer and stalling characteristics of NACA 64a010 airfoil section
Engineering Index Backfile | 1950
|Engineering Index Backfile | 1950
|Engineering Index Backfile | 1949
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