The results of numerical simulation of sonic boom near field flow around the NASA Concept 25D (C25D) low-boom supersonic demonstrator configuration are presented. The calculations were carried out for a stationary flow of an ideal gas in a three-dimensional mode with a help of SOLIDWORKS Flow Simulation solver. Comparison with the results of numerical simulations obtained by researchers in the framework of the 2nd AIAA Sonic Boom Prediction Workshop is made.


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    Title :

    Numerical simulation of sonic boom near-field flow over C25D model


    Contributors:

    Conference:

    INTERNATIONAL CONFERENCE ON THE METHODS OF AEROPHYSICAL RESEARCH (ICMAR 2020) ; 2020 ; Novosibirsk, Russia


    Published in:

    Publication date :

    2021-05-24


    Size :

    5 pages





    Type of media :

    Conference paper


    Type of material :

    Electronic Resource


    Language :

    English



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