Wind-tunnel investigation of an NACA 23012 airfoil with two sizes of balanced split flap
Wartime report ; L-441
1940
13 S., [20] Bl
graph. Darst
Originally issued November 1940 as Advance confidential report
Report
Englisch
Wind-tunnel investigation of NACA 23012 airfoil with two sizes of balanced split flap
Engineering Index Backfile | 1940
|Wind-tunnel investigation of NACA 23012 airfoil with 0.30-airfoil-chord double slotted flap
Engineering Index Backfile | 1943
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