Results of measurement in maneuvering flight analyzed and found to verify fact that knowledge of tail load parameters will permit calculation of horizontal tail load; critical conditions for design enumerated.


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    Title :

    Flight measurements of aerodynamic loads on horizontal tail surface of fighter-type airplane


    Additional title:

    Nat Advisory Commitee Aeronautics -- Tech Note


    Contributors:


    Publication date :

    1947


    Size :

    55 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English