This paper presents the results of a study that used a three-dimensional transonic analysis method to analyze flow around a wing-mounted prop-fan configuration. The transonic analysis method employs a cell-oriented finite volume approach to solve the full potential equation in conservative form over a numerically generated surface-fitted grid. The propeller slipstream effects are simulated using a linearized transpiration boundary condition. The results of analyses of flow over clean wing/body, wing/body/nacelle, and wing/body nacelle with slipstream are compared to test data.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Transonic flow simulation of prop-fan configurations


    Beteiligte:
    Samant, S. S. (Autor:in) / Yu, N. J. (Autor:in) / Rubbert, P. E. (Autor:in)

    Kongress:

    American Institute of Aeronautics and Astronautics, Aerospace Sciences Meeting ; 1983 ; Reno, NV


    Erscheinungsdatum :

    01.01.1983


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Transonic flow simulation of prop-fan configurations

    SAMANT, S. / YU, N. / RUBBERT, P. | AIAA | 1983



    Efficient Euler analysis of transonic flow around advanced turbo-prop

    Dong-Ho, Lee / Oh-Hyun, Rho / Chang-Joo, Kim | Tema Archiv | 1990


    Efficient Euler Analysis of Transonic Flow Around Advanced Turbo-Prop

    Kim, Chang-Joo / Lee, Dong-Ho / Rho, Oh-Hyun | SAE Technical Papers | 1990