A boundary-layer integral approach is combined with a finite-difference relaxation method to calculate viscous interactions between separated flows at subsonic and transonic velocities. Results are obtained for separated laminar flows on circular-arc airfoils at zero angle of attack and are compared with data of Collins (1972). Inviscid and viscous flows are covered.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Calculation of separated flows at subsonic and transonic speeds


    Beteiligte:
    Klineberg, J. M. (Autor:in) / Steger, J. L. (Autor:in)

    Kongress:

    International Conference on Numerical Methods in Fluid Mechanics ; 1972 ; Paris, France


    Erscheinungsdatum :

    01.01.1973


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    A study of isolated nacelle flows at subsonic and transonic speeds

    Humphries, P. / Gillan, M. / Raghunathan, S. | AIAA | 1998


    A Study of Isolated Nacelle Flows at Subsonic and Transonic Speeds

    Humphries, P. / Gillan, M. / Raghunathan, S. et al. | British Library Conference Proceedings | 1998



    Mean and Fluctuating Pressure in Boat-Tail Separated Flows at Transonic Speeds

    Rajan Kumar / P. R. Viswanath / A. Prabhu | AIAA | 2002