A wall-injected, hydrogen-fueled scramjet is modeled numerically using a parabolic Navier-Stokes computer code with a k-epsilon turbulence model and finite-rate chemistry. The numerical results are compared to experimental scramjet data taken in a shock tunnel and are found to be in reasonable agreement. Under the conditions studied, the numerical results show that combustion in the scramjet is mainly mixing limited.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Numerical modeling of wall-injected scramjet experiments


    Beteiligte:

    Erschienen in:

    Erscheinungsdatum :

    1993-04-01



    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Numerical modeling of wall-injected scramjet experiments

    BRESCIANINI, C. P. / MORGAN, R. G. | AIAA | 1993


    Numerical Modeling of Wall-Injected Scramjet Experiments

    Brescianini, C.P. | Online Contents | 1993



    Investigation of an Intake Injected Hot Wall Scramjet

    Kovachevich, Anne / Paull, Allan / McIntyre, Timothy | AIAA | 2004


    INVESTIGATION OF AN INTAKE INJECTED HOT-WALL SCRAMJET

    Kovachevich, A. / Paull, A. / McIntyre, T. et al. | British Library Conference Proceedings | 2004