From power spectral techniques, frequency-response functions are obtained for deflection and twist responses at three spanwise locations to vertical gusts, and results compared with those obtained for reference quasi-static aircraft; analysis of effects of deflection velocity and twisting motions on local angles of attack.


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    Title :

    Analysis of flight-test measurements of wing structural deformations in rough air of large flexible swept-wing airplane


    Additional title:

    NASA -- Memo


    Contributors:


    Publication date :

    1959


    Size :

    46 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :