Wind-tunnel investigation of an NACA 23012, 23021 and 23030 airfoils with various sizes of split flap
1939
13 S.
graph. Darst.
Buch
Englisch
Wind-tunnel investigation of NACA 23012 airfoil with two sizes of balanced split flap
Engineering Index Backfile | 1940
|Engineering Index Backfile | 1939
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