Results of an investigation of a dynamic model in the Langley 20-foot free-spinning tunnel are presented. Erect spin and recovery characteristics were determined for a range of mass distributions and center-of-gravity positions. The effects of lateral displacement of the center of gravity, engine rotation, nose strakes, and increased rudder area were investigated.


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    Title :

    Free-Spinning-Tunnel Investigation of a 1/17 Scale Model of the Cessna T-37A Airplane


    Contributors:

    Publication date :

    1958-01-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English


    Keywords :