Study made to investigate effect of slipstream span on lift increment due to thrust on wing with high lift flaps; comparison with results obtained on same model with two propellers showed that lift increment due to thrust was proportional to slipstream velocity and proportional to wing area in slipstream.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Large-scale wind-tunnel tests of airplane model with unswept, aspect-ratio-10 wing, four propellers, and blowing flaps


    Weitere Titelangaben:

    NASA -- Tech Note


    Beteiligte:
    Weiberg, J.A. (Autor:in) / Page, V.R. (Autor:in)


    Erscheinungsdatum :

    1959


    Format / Umfang :

    39 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :