Wind-tunnel investigation of an NACA 23012 airfoil with two sizes of balanced split flap
01.11.1940
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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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