Abstract:This work presents a framework for the optimisation of certain aspects of a BERPlike rotor blade in forward flight while constraining hover performance. The proposed method employs a high-fidelity, efficient CFD technique that uses the Harmonic Balance method in conjunction with artificial neural networks (ANNs) as metamodels, and genetic algorithms (GAs) for optimisation. The approach has been previously demonstrated for the optimisation of linear twist of rotors in hover (steady case) and the optimisation of… Show more
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