A unified approach which makes it possible to determine the extent and onset of transition in one calculation is presented. It treats the laminar fluctuations in a manner similar to that used in describing turbulence. As a result, the complete flowfield can be calculated using existing CFD codes and without the use of stability codes. The method is validated by comparing the results for flat plates, airfoils, and infinite swept wings with available experiments. In general, good agreement is indicated.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    A Transition Closure Model for Predicting Transition Onset


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:

    Kongress:

    World Aviation Congress & Exposition ; 1997



    Erscheinungsdatum :

    01.10.1997




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Transition Closure Model for Predicting Transition Onset

    E. S. Warren / H. A. Hassan | AIAA | 1998


    A Transition Closure Model for Predicting Transition Onset

    Warren, E. S. / Hassan, H. A. / SAE et al. | British Library Conference Proceedings | 1997


    A transition closure model for predicting transition onset

    Warren, Eric / Hassan, Hassan | AIAA | 1997



    Parallel Compatible Transition Closure Model for High-Speed Transitional Flow

    Xu, Jiakuan / Bai, Junqiang / Fu, Ziyuan et al. | AIAA | 2017