Wind tunnel investigation of an NACA 23021 airfoil with two arrangements of a 40 percent chord slotted flap
N.A.C.A. 40-percent-chord wind-tunnel
1939
11, [11] Bl.
Miscellaneous
English
RVK: | ZO 7000 |
Engineering Index Backfile | 1939
|Engineering Index Backfile | 1941
|Wind-tunnel investigation of NACA 23012 airfoil with 0.30-airfoil-chord double slotted flap
Engineering Index Backfile | 1943
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