Investigation made in Langley 15-ft free spinning tunnel.


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    Title :

    Effect of horizontal-tail position on hinge moments of unbalanced rudder in attitudes simulating spin conditions, R


    Additional title:

    Nat Advisory Committee Aeronautics -- Tech Note


    Contributors:


    Publication date :

    1947


    Size :

    13 pages


    Remarks:

    51 Supp Plates


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English