This paper present the effect of using a more detailed model for the computation of the range, when it is used as objective for the multidiciplinary optimization of a transonic wing of a business jet. The new formulation considers the change of angle of attack that the aircraft must follow during cruise.
High Fidelity Aero-Structural Optimization of a Wing Using a Step-Range Approach
Scaramuzzino, P. F.;QUARANTA, GIUSEPPE
2017-01-01
Abstract
This paper present the effect of using a more detailed model for the computation of the range, when it is used as objective for the multidiciplinary optimization of a transonic wing of a business jet. The new formulation considers the change of angle of attack that the aircraft must follow during cruise.File in questo prodotto:
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