Multi-objective aerodynamic optimization design of variable camber leading and trailing edge of airfoil

Variable camber is an effective method for improving the flight efficiency of large aircraft, and has attracted the attention of researchers. This work focused on the optimization of a variable camber airfoil. First, the influences of the variable camber of the leading and trailing edges on the airf...

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Veröffentlicht in:	Proceedings of the Institution of Mechanical Engineers. Part C, Journal of mechanical engineering science Journal of mechanical engineering science, 2022-05, Vol.236 (9), p.4748-4765
Hauptverfasser:	Bao, Nvzi, Peng, Yehui, Feng, Heying, Yang, Chenghao
Format:	Artikel
Sprache:	eng
Schlagworte:	Aerodynamic coefficients Aerodynamics Aircraft Aircraft design Airfoils Angle of attack Artificial neural networks Camber Computational fluid dynamics Deflection Design optimization Drag Genetic algorithms Iterative algorithms Iterative methods Leading edges Mathematical analysis Mathematical models Multiple objective analysis Neural networks Noise levels Noise reduction Optimization Prediction models Rotation Trailing edges Two dimensional models Wings (aircraft)
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