Flight investigation of boundary-layer control by suction slots on an NACA 35-215 low-drag airfoil at high Reynolds numbers
Wartime report ; L-521
1944
18 S., [15] Bl
Ill., graph. Darst
Originally issued February 1944 as Advance confidential report 4B29
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Report
English
Experimental investigation of NACA 63-012 airfoil section with leading-edge suction slots
Engineering Index Backfile | 1948
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