Continuum methods are used to analyze the stagnation flow field of the aeroassist flight experiment (AFE) vehicle. For the lower altitude portion of an AFE trajectory, the viscous shock-layer equations are employed. At higher altitudes, the full Navier-Stokes equations with chemical nonequilibrium and surface slip are used. Particular attention is given to the effect of surface catalyticity on surface heating, electron number density, and flow field structure.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Stagnation flow field analysis for an aeroassist flight experiment vehicle


    Beteiligte:
    Gupta, Roop N. (Autor:in) / Simmonds, Ann L. (Autor:in)

    Erscheinungsdatum :

    01.06.1988


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :



    Flight stagnation-point heating calculations on Aeroassist Flight Experiment vehicle

    Hamilton, H. H., II / Gupta, Roop N. / Jones, Jim J. | NTRS | 1991


    Flight stagnation-point heating calculations on Aeroassist Flight Experiment vehicle

    HAMILTON, H. H. / GUPTA, ROOP N. / JONES, JIM J. | AIAA | 1991


    The Aeroassist Flight Experiment

    Walberg, G. D. / Siemers, P. M., III / Calloway, R. L. et al. | NTRS | 1987


    Aeroassist Flight Experiment (AFE)

    Siemers, Paul M., III | NTRS | 1988