Results of investigation made in NACA 7 by 10-ft wind tunnel; static rolling and yawing moments were determined for all devices tested, and static hinge moments and time response were determined for few devices of each type.
Wind-tunnel investigation of spoiler, deflector, and slot lateral-control devices on wings with full-span split and slotted flaps
Nat Advisory Committee Aeronautics -- Report
1941
30 pages
Report
English
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Engineering Index Backfile | 1942
|Engineering Index Backfile | 1946
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