Study of influence of Hall effect on magnetogasdynamic flow around nose of blunt body; local similarity is applied to stagnation region of attached shock layer generated in hypersonic flow about blunt body containing magnetic dipole source; electrically conducting and insulated bodies are considered; typical current path lines are shown for conducting and insulated bodies, respectively; conducting body is found to have greater shock standoff, drag, and rolling-moment coefficient than insulated body.


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    Titel :

    Hall effect in flight magnetogasdynamics


    Weitere Titelangaben:

    AIAA J


    Beteiligte:
    Porter, R.W. (Autor:in) / Cambel, A.B. (Autor:in)

    Erschienen in:

    AIAA Journal ; 5 , n 12


    Erscheinungsdatum :

    1967


    Format / Umfang :

    6 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



    Hall effect in flight magnetogasdynamics.

    Cambel, A. B. / Porter, R. W. | NTRS | 1967



    Numerical Modeling of the Hall Effect in Re-Entry Magnetogasdynamics

    Poggie, Jonathan / Gaitonde, Datta | AIAA | 2002


    One-dimensional magnetogasdynamics.

    KAUL, C. N. | AIAA | 1967