The existing two-dimensional Euler code is extended to the three-dimensional flow problem in which the transonic flow around the double fin-body combinations was analysed. Ni's two-dimensional formulas are extended to the three-dimensional case and applied to the supersonic flow calculation over the double fin-body combinations.The numerical results have proved to be very accurate in predicting the pressure distribution and capturing the shock. The code extended to the three-dimensional flow analysis in the paper can be consequently used to estimate the aerodynamic characteristics of the complicated body.


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    Title :

    Numerical Anaylsis of Compressible Flow Around Three-Dimensional Fin-Body Combination


    Additional title:

    Sae Technical Papers


    Contributors:
    Kim, Chong Am (author) / Lee, Dong Ho (author) / Rho, Ohyun (author) / Kim, Won Wook (author)

    Conference:

    Aerospace Technology Conference and Exposition ; 1990



    Publication date :

    1990-09-01




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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