Flight test data obtained at altitude of 5000 ft are analyzed to determine effects of airplane vertical translation and pitching motions; power spectral techniques used to determine contributions of these motions to angles of attack; results compared with direct gust induced angle of attack.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Experimental measurements of effects of airplane motions on wing and tail angles of attack of swept-wing bomber in rough air


    Additional title:

    NACA -- Tech Note


    Contributors:
    Engel, J.N. (author)


    Publication date :

    1958


    Size :

    25 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :