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- W2173070897 abstract "A rapid, accurate and robust methodology to optimise high lift devices settings on a exible wing has been developed. A quasi-3D approach has been used to evaluate the aerodynamic performance of the wing: two-dimensional viscous data from a panel coupled boundary layer code are used as inputs for a lifting surface method. Flexibility effects are included by mean of a reduced structural model. Firstly, the rapid method is validated against available wind tunnel data for the KH3Y test case; secondly, the slat and ap settings are optimised for landing requirements using a multi-objective optimisation algorithm. The results obtained have shown the appli- cability of such methods to the optimisation of high lift configurations, providing both the accuracy and efficiency required at the preliminary design stage." @default.
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- W2173070897 date "2013-01-01" @default.
- W2173070897 modified "2023-09-27" @default.
- W2173070897 title "Aerodynamic optimisation of a flexible high-lift wing" @default.
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