Positions of boundary layer transition were ascertained for sweptback and straight wing of like conditions; sweptback wing in definite range of angle of attack resulted in backward shift of transition point on suction side of wing; favorable effect of sweepback on position of transition point predicted by LIPPISCH is confirmed. English translation from (ZWB) Deutsche Luftfahrtforschung -- U u M n 3151 Sept 13 1944.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Maintaining laminar flow in boundary layer using swept-back wing


    Weitere Titelangaben:

    Nat Advisory Committee Aeronautics -- Tech Memo


    Beteiligte:
    Brennecke (Autor:in)


    Erscheinungsdatum :

    1948


    Format / Umfang :

    9 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :




    Electrogasdynamic laminar flow control on a swept wing

    Chernyshev, Sergey L | Online Contents | 2016


    Large-eddy simulation of laminar-turbulent transition in a swept-wing boundary layer

    Huai, Xiaoli / Piomelli, Ugo / Joslin, Ronald | AIAA | 1997


    Large-Eddy Simulation of Laminar-Turbulent Transition in a Swept-Wing Boundary Layer

    Huai, X. / Joslin, R. D. / Piomelli, U. et al. | British Library Conference Proceedings | 1997