A three-dimensional, Reynolds-averaged Navier-Stokes code has been used to numerically analyze flow through a two-strut, supersonic combustion ramjet (scramjet) inlet configuration. It solves the governing equations in full conservation form using either a fully explicit or explicit-implicit method. An algebraic, two-layer eddy-viscosity model is used for turbulent flow calculations. The analysis allows inclusion of end effects that are caused by the aft placement of the cowl on the underside of the inlet. A special grid has been developed to accommodate the struts embedded in the inlet flowfield. Detailed numerical results are presented here for the two-strut configuration, and a comparison is made with the available experimental results.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Numerical simulation of flow through a two-strut scramjet inlet


    Beteiligte:
    Kumar, Ajay (Autor:in)


    Erscheinungsdatum :

    01.06.1989



    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :




    Aerodynamic Performance of Scramjet Inlet Models with a Single Strut

    Kouichiro Tani / Takeshi Kanda / Kenji Kudo | AIAA | 2006


    Aerodynamic performance of scramjet inlet models with a single strut

    TAI, KOUICHIRO / KANDA, TAKESHI / KUDOU, KENJI et al. | AIAA | 1993


    Numerical Simulation of Flow through Scramjet Inlet - Isolator Model with Pressure Feedback

    Sarout, Yuvraj / R, Thundil Karuppa Raj / Paramasivam, Senthilkumar | AIAA | 2020