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High-Fidelity and High-Performance Laminar Wing Optimization (HIPERLAM)

Date du début: 1 sept. 2012, Date de fin: 30 juin 2014,

"Proposed work aims at developing efficient optimization tools for NLF design where the cost function is the total drag (pressure and friction). The tool utilizes efficient and accurate computation of gradients of objective functions as well as robust parametrization of the geometry. Our approach uses Computational Fluid Dynamics followed by accurate boundary-layer stability analysis in order to f ...
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