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After describing a multi-fidelity surrogate model, based on Kriging and Co-Kriging, an aerodynamic optimization on a helicopter rotor blade is presented and analyzed.
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This page is a summary of: Multifidelity Aerodynamic Optimization of a Helicopter Rotor Blade, AIAA Journal, August 2019, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.j056513.
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