Method for applying deformation relations derived in NAE Laboratory Report LR-28 for wings without taper, to analysis of wings with moderate degree of taper; by way of illustration, experimental results for wing models of cellulose acetate yawed at 0,30,45, and 60 ° were used. (received 1955)


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    Title :

    Deformation analysis of tapered swept wings


    Additional title:

    Canada. Nat Aeronautical Establishment -- Report


    Contributors:
    Hall, A.H. (author)


    Publication date :

    1953


    Size :

    12 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :