Theoretical Analyses to Determine Unbalanced Trailing-Edge Controls Having Minimum Hinge Moments Due to Deflection at Supersonic Speeds.


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    Title :

    Theoretical analyses to determine unbalanced trailing-edge controls having minimum hinge moments due to deflection at supersonic speeds


    Additional title:

    NACA -- Tech Note


    Contributors:
    Goin, K.L. (author)


    Publication date :

    1955


    Size :

    52 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :