Tests made on 32-ft whirling arm of Daniel Guggenheim Airship Institute of tapered wing to determine rolling and yawing moments due to angular velocity in yaw; results given in form of span load distributions and in calculated moment coefficients.
Pressure-distribution measurements on tapered wing with full-span split flap in curved flight
Nat Advisory Committee Aeronautics -- Tech Note
1939
8 pages
8 supp sheets, Bibliography
Report
English
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Pressure distribution measurements on tapered wing with partial-span split flap in curved flight
Engineering Index Backfile | 1939
|Pressure-distribution measurements on rectangular wing with partial-span split flap in curved flight
Engineering Index Backfile | 1939
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