Computational Investigation of Vortex Breakdown over a Pitching Delta Wing at Supersonic Speeds
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DOI: 10.24200/sci.2017.4246
Abstract: Vortex breakdown in compressible flows over a 60-degrees sweep delta wing with a sharp leading edge undergoing pitching oscillations is computationally studied. Emphasis in this study is on possible supersonic vortex breakdown for pitching motion… read more here.
Keywords: investigation vortex; breakdown pitching; pitching delta; computational investigation ... See more keywords