Weimin Sang

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Ice accretion leads to significant deterioration of aircraft aerodynamic performance and handling qualities. In this paper, ice accretion on NACA 0012 airfoil and multi-element airfoils are predicted using CFD method. Using a multi-block grid technique, we generate computational grids for the multi-element airfoils. A four-stage Runge-Kutta method is used(More)
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