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Unsteady parametrization of a morphing wing design for improved aerodynamic performance

Abdessemed, Chawki; Yao, Yufeng; Narayan, Pritesh; Bouferrouk, Abdessalem

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Authors

Chawki Abdessemed

Yufeng Yao Yufeng.Yao@uwe.ac.uk
Professor in Aerospace Engineering



Abstract

A morphing wing is a bio-inspired concept where all moving parts e.g. slats/flaps are replaced with a deformable body. This paper describes a methodology that uses modified parametrization methods to define a morphing geometry, and applies user-defined function (UDF) to generate dynamic meshing around it for unsteady flow analysis. To verify mesh quality during deformation, steady CFD results of a deformed mesh at a
‘frozen’ time-step were compared to those from a regenerated
mesh over a range of angles of attack. It was found that results from a deformed and re-generated mesh are in good agreement, confirming the validity of dynamic meshing. Furthermore, a comparison study between a morphed and flapped airfoil was performed, where it was observed that the morphed airfoil produced higher lift/drag ratio than the flapped one. Finally, an unsteady CFD analysis was conducted using the
developed UDF as a proof of concept study for further
research.

Citation

Abdessemed, C., Yao, Y., Narayan, P., & Bouferrouk, A. (2017, March). Unsteady parametrization of a morphing wing design for improved aerodynamic performance. Paper presented at 52nd 3AF International Conference on Applied Aerodynamics, Lyon, France

Presentation Conference Type Conference Paper (unpublished)
Conference Name 52nd 3AF International Conference on Applied Aerodynamics
Conference Location Lyon, France
Start Date Mar 27, 2017
End Date Mar 29, 2017
Acceptance Date Dec 14, 2016
Deposit Date Feb 27, 2017
Publicly Available Date Oct 3, 2017
Peer Reviewed Not Peer Reviewed
Keywords unsteady, parametrization, morphing, wing, design, improved, aerodynamic, performance
Public URL https://uwe-repository.worktribe.com/output/904795
Additional Information Title of Conference or Conference Proceedings : 52nd 3AF International Conference on Applied Aerodynamics

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