Method for calculation of supersonic axially symmetric flow of perfect gas around given blunt body involves iteration of solution of inverse problem, and matches bluntness of calculated body at nose with that of given one; solution of inverse problem is carried out; rational approximations are obtained for flow quantities on body in terms of arc length measured from nose; computing time on IBM 7090 is about 60 msec for solution of inverse problem, and less than second for direct problem; good agreement with measurements and other calculations is found in subsonic region when bluntness of given body is less than or equal to that of sphere.


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    Titel :

    Use of rational approximations in calculation of flows past blunt bodies


    Weitere Titelangaben:

    AIAA J


    Beteiligte:
    Van Tuyl, A.H. (Autor:in)

    Erschienen in:

    AIAA Journal ; 5 , n 2 ; p 218-225


    Erscheinungsdatum :

    1967


    Format / Umfang :

    8 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :




    Direct Monte Carlo Simulations of Hypersonic Flows Past Blunt Bodies

    Weaver, D. P. / Campbell, D. H. / Muntz, E. P. | AIAA | 1989


    Heat Transfer Calculation of Blunt Bodies in Nonequilibrium Air Flows

    Hamamoto, N. / Lee, M. G. / Nakamura, Y. et al. | British Library Conference Proceedings | 1997