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Combined aerostructural wing and high-lift system optimization

Combined aerostructural wing and high-lift system optimization
Combined aerostructural wing and high-lift system optimization
A coupled-adjoint aerostrutctural wing optimization tool has been modified to include the optimization of high-lift devices from the start of the optimization process. The aerostructural tool couples a quasi-three-dimensional method with a finite beam element model. In this paper, the quasi-three-dimensional method is modified using a α method of Van Dam to enable high-lift aerodynamic analysis...
American Institute of Aeronautics and Astronautics
Van Den Kieboom, K.
f0346825-60d8-4aa6-a7f9-ef95135d3c63
Elham, A.
676043c6-547a-4081-8521-1567885ad41a
Van Den Kieboom, K.
f0346825-60d8-4aa6-a7f9-ef95135d3c63
Elham, A.
676043c6-547a-4081-8521-1567885ad41a

Van Den Kieboom, K. and Elham, A. (2016) Combined aerostructural wing and high-lift system optimization. In 17th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference. American Institute of Aeronautics and Astronautics.. (doi:10.2514/6.2016-3510).

Record type: Conference or Workshop Item (Paper)

Abstract

A coupled-adjoint aerostrutctural wing optimization tool has been modified to include the optimization of high-lift devices from the start of the optimization process. The aerostructural tool couples a quasi-three-dimensional method with a finite beam element model. In this paper, the quasi-three-dimensional method is modified using a α method of Van Dam to enable high-lift aerodynamic analysis...

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Published date: 10 June 2016
Venue - Dates: 17th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference, , Washington D.C., United States, 2016-06-13 - 2016-06-17
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Local EPrints ID: 471024
URI: http://eprints.soton.ac.uk/id/eprint/471024
DOI: doi:10.2514/6.2016-3510
PURE UUID: 40aa2dea-f56f-4532-bef6-6f61712a8859

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Date deposited: 24 Oct 2022 17:04
Last modified: 16 Mar 2024 21:27

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Contributors

Author: K. Van Den Kieboom
Author: A. Elham

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