Two-dimensional wind-tunnel investigation of two NACA low-drag airfoil sections equipped with slotted flaps and a plain NACA low-drag airfoil section for XF6U-1 airplane
Wartime report ; L-746
1946
9 S., [7] Bl
graph. Darst
Originally issued January 1946 as Memorandum report L5L11
Report
Englisch
Engineering Index Backfile | 1947
|Wind-tunnel investigation of NACA 23012 airfoil with 0.30-airfoil-chord double slotted flap
Engineering Index Backfile | 1943
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