The performance and static stability and control characteristics of the Ryan Flex-Wing airplane were determined in an investigation conducted in the Langley full-scale tunnel through an angle-of-attack range of the keel from about 14 to 44 deg. for power-on and -off conditions. Comparisons of the wind-tunnel data with flight-test data obtained with the same airplane by the Ryan Aeronautical Company were made in a number of cases.
Summary of Results Obtained in Full-Scale Tunnel Investigation of the Ryan Flex-Wing Airplane
1962-08-14
Report
No indication
English
Investigation of structural damping of full-scale airplane wing
Engineering Index Backfile | 1952
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