A previously published real-time simulation algorithm, the matrix stability region placement (MSRP) method, is used to simulate a small perturbation model of the NASA Lewis Mach 2.5 40-60 mixed compression inlet. The model is representative of high-speed internal flow propulsion systems which can be approximated as quasi-one-dimensional flows. The resulting system of equations, which is stiff, is also simulated by the second-order Adam-Bashforth method. It is shown that the MSRP method can be used to simulate small perturbation models of high-speed internal flow propulsion systems in real time.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Real-time simulation of supersonic inlets


    Beteiligte:

    Kongress:

    IEEE International Conference on Systems Engineering ; 1990 ; Pittsburgh, PA, United States


    Erscheinungsdatum :

    01.01.1990


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Real-time simulation of supersonic inlets

    Mossayebi, F. / Pansino, S.R. / Hartley, T.T. et al. | Tema Archiv | 1990


    Numerical Simulation For Supersonic Inlets

    Varner, M. O. / Martindale, W. R. / Phares, W. J. et al. | NTRS | 1987


    Supersonic cruise inlets

    Bowditch, D. N. / Coltrin, R. E. / Sanders, B. W. et al. | NTRS | 1971


    Inlets for supersonic missiles

    Mahoney, John J. | TIBKAT | 1990


    Flow fields in supersonic inlets

    Sorensen, V. L. | NTRS | 1979