Multi Objective Optimization of Transonic Airfoil Using Cst Methodology with General and Evolved Supercritical Class Function

Abstract

CST method is a powerful parameterization method because of its simplicity, robustness, and its ability to be generalized into various possible shapes of aerodynamic bodies. The geometry from CST itself is mainly determined by the formula of class and shape function. Application of CST to transonic airfoil optimization is still rare and more studies are… (More)

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