Wind-tunnel investigation of an NACA 23012 airfoil with a 30-percent-chord Maxwell slat and with trailing-edge flaps
Wartime report ; L-693
1941
10 S., [8] Bl
graph. Darst
Originally issued June 1941 as Memorandum report
Report
Englisch
Wind-tunnel investigation of NACA 23012 airfoil with 30-percent-chord venetian-blind flaps
Engineering Index Backfile | 1942
|