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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    Title :

    Hall effect in flight magnetogasdynamics


    Additional title:

    AIAA J


    Contributors:
    Porter, R.W. (author) / Cambel, A.B. (author)

    Published in:

    AIAA Journal ; 5 , n 12


    Publication date :

    1967


    Size :

    6 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :



    Hall effect in flight magnetogasdynamics.

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