Search Results - A. G. Golubev

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    FEATURES OF THE SUBSONIC WIND TUNNEL EXPERIMENT WITH ROTATING MODELS OF AIRCRAFT

    FEATURES OF THE SUBSONIC WIND TUNNEL EXPERIMENT WITH ROTATING MODELS OF AIRCRAFT by A. G. Golubev, A. A. Michkin, E. G. Stolyarova

    Published 2016-11-01
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  2. 2
    APPLICABILITY OF THE OPEN SOURCE PACKAGE OPENFOAM FOR NUMERICAL MODELING SEPARATED FLOW AROUND AN AIRCRAFT AT SUBSONIC AND SUPERSONIC SPEEDS

    APPLICABILITY OF THE OPEN SOURCE PACKAGE OPENFOAM FOR NUMERICAL MODELING SEPARATED FLOW AROUND AN AIRCRAFT AT SUBSONIC AND SUPERSONIC SPEEDS by V. T. Kalugin, A. G. Golubev, A. S. Epikhin, A. A. Michkin

    Published 2017-01-01
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