Results of investigation of dynamic model in Langley 20-ft free spinning tunnel; erect and inverted spin characteristics were determined for range of mass distribution conditions; recovery from spins obtained was attempted by various control manipulations.


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    Title :

    Free-spinning-tunnel investigation of 1/20-scale model of unswept-wing jet-propelled trainer airplane


    Additional title:

    NASA -- Tech Note


    Contributors:


    Publication date :

    1960


    Size :

    18 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :