Wind-tunnel investigation of an NACA 23012 airfoil with an 18.05-percent-chord Maxwell slat and with trailing-edge flaps
Wartime report ; L-574
1941
9 S., [8] Bl
graph. Darst
Originally issued October 1941 as Memorandum report
Report
Englisch
Wind-tunnel investigation of NACA 23012 airfoil with 30-percent-chord venetian-blind flaps
Engineering Index Backfile | 1942
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