Wind-tunnel investigation of an NACA 66-series 16-percent-thick low-drag tapered wing with Fowler and split flaps
Wartime report ; L-134
1946
11 S., [9] Bl
graph. Darst
Originally issued January 1946 as Advance confidential report L5F28
Report
Englisch
Engineering Index Backfile | 1946
|Wind-tunnel investigation of NACA 23012 airfoil with 30-percent-chord venetian-blind flaps
Engineering Index Backfile | 1942
|Engineering Index Backfile | 1941
|