Subject is important in study of aircraft dynamic stability; solution in closed form found; polar representation of downwash at given distance behind wing is divergent spiral; at large distances behind wing downwash variation with distance is sinusoidal.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Downwash behind two-dimensional wing oscillating in plunging motion


    Additional title:

    J Aeronautical Sciences


    Contributors:
    Lapin, E. (author) / Crookshanks, R. (author) / Hunter, H.F. (author)


    Publication date :

    1952


    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, Warter H , Jr | NTRS | 1955


    Prediction of downwash behind swept-wing airplanes at subsonic speed

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