Publication Date:
2019-08-17
Description:
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.
Keywords:
Aerodynamics
Type:
NASA-TM-SX-727
,
L-3093
Format:
application/pdf
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