Wind-tunnel investigation of an NACA 23021 airfoil with two sizes of balanced split flaps
Wartime report ; L-449
1941
13 S., [19] Bl
graph. Darst
Originally issued February 1941 as Advance confidential report
Digital preservation by Technische Informationsbibliothek (TIB) / Leibniz-Informationszentrum Technik und Naturwissenschaften und Universitätsbibliothek
Report
English
Wind-tunnel investigation of NACA 23021 airfoil with two sizes of balanced split flaps
Engineering Index Backfile | 1941
|Wind-tunnel investigation of N.A.C.A. 23021 airfoil with various arrangements of slotted flaps
Engineering Index Backfile | 1939
|Wind-tunnel investigation of NACA 23012 airfoil with two sizes of balanced split flap
Engineering Index Backfile | 1940
|