Tests made on 32-ft whirling arm of Daniel Guggenheim Airship Institute of rectangular wing of NACA 23012 section to determine rolling and yawing moment due to angular velocity in yaw.
Pressure-distribution measurements on rectangular wing with partial-span split flap in curved flight
Nat Advisory Committee Aeronautics -- Tech Note
1939
7 pages
8 Supp sheets
Report
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Pressure distribution measurements on tapered wing with partial-span split flap in curved flight
Engineering Index Backfile | 1939
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