Loads measured on the horizontal tail, vertical tail, and wing and the aeroelastic distortions of elevators, stabilizers, and fuselage of a B-45A airplane in a right and left roll at a Mach number of 0.60 and an altitude of 15,000 feet are presented. The data are given in time-history form.


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    Title :

    Time Histories of Loads and Deformation on a B-45A Airplane in Two Aileron Rolls


    Contributors:

    Publication date :

    1949


    Size :

    25 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English