Wind-Tunnel Investigation of Control-Surface Characteristics XVII : Beveled-Trailing-Edge Flaps of 0.20, 0.30, and 0.40 Airfoil Chord on an NACA 0009 Airfoil
1944-04-01
Miscellaneous
No indication
English
Engineering Index Backfile | 1948
|Engineering Index Backfile | 1948
|Wind-tunnel investigation of NACA 23012 airfoil with 0.30-airfoil-chord double slotted flap
Engineering Index Backfile | 1943
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