By application of semirigid analysis divergence speed coefficient is obtained in form of two factors involving modes of deformation and downwash; results in case of normal plain wings are illustrated by curves of divergence speed factor as function of taper ratio.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Estimation of wing torsional divergence speed with downwash correction


    Additional title:

    Nat Research Council Canada -- Aeronautical Note


    Contributors:
    Hall, A.H. (author)


    Publication date :

    1948


    Size :

    7 pages


    Remarks:

    2 supp p


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :



    Calculation of downwash behind wing

    Multhopp, H. | Engineering Index Backfile | 1938


    Prediction of downwash behind swept-wing airplanes at subsonic speed

    DeYoung, J. / Barling, Jr., W.H. | Engineering Index Backfile | 1955


    Prediction of downwash behind swept-wing airplanes at subsonic speed

    DeYoung, John / Barling, Walter H. | TIBKAT | 1955


    Prediction of Downwash Behind Swept-wing Airplanes at Subsonic Speed

    Deyoung, John / Barling, Warter H , Jr | NTRS | 1955