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.


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    Title :

    Summary of Results Obtained in Full-Scale Tunnel Investigation of the Ryan Flex-Wing Airplane


    Contributors:

    Publication date :

    1962-08-14


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English


    Keywords :