Evolutionary airfoil shape optimization coupling parameterization methods with lagrangian vortex method
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In this paper, evolutionary optimization procedures for the aircraft’s airfoil family during level flight (low angle of attack) are discussed. That is because in other flight conditions, such as take-off, climb, descend, landing, the level flight condition takes most of the time of economic flight.
Nội dung trích xuất từ tài liệu:
Evolutionary airfoil shape optimization coupling parameterization methods with lagrangian vortex method
Nội dung trích xuất từ tài liệu:
Evolutionary airfoil shape optimization coupling parameterization methods with lagrangian vortex method
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