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Effects of a gurney flap were numerically investigated on the supercritical NASA airfoil by solving the two-dimensional Reynolds-averaged Navier-Stokes equations for a range of transonic Mach numbers and angles of attack, using turbulence compressibl
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https://explore.openaire.eu/search/publication?articleId=doi_dedup___::df279c4f12a3ba1fcedd98007024902b