Investigating aileron design for ultra-high aspect ratio wings
Investigating aileron design for ultra-high aspect ratio wings
The Strut-Braced Wing (SBW) is a promising configuration for achieving next-generation sustainable and fuel-efficient aviation goals by using a composite Ultra-High Aspect Ratio Wing (UHARW) design. UHARW is more flexible than conventional wings, so the aileron effectiveness is a key constraint in the design and optimization of UHARW to avoid aileron reversal. This paper presents an aileron design methodology for UAHRW design and optimization by integrating the aileron’s required roll moment into a coupled adjoint aerostructural optimization tool for the aeroelastic and aerostructural investigations of the SBW configuration. The aeroelastic optimization results show that it is necessary to take into account aileron design variables in aeroelastic optimization as the wing structural weight can be reduced further. The aerostructural optimization results show a significant performance improvement of the SBW aircraft with considering the aileron design variables. The optimized SBW with two ailerons has significantly lower fuel weight and MTOW than the optimized SBW with only one aileron design. For both cases, the optimizer significantly reduces the wing drag by weakening/removing shock waves.
American Institute of Aeronautics and Astronautics
Ma, Yiyuan
ccea8698-10f9-4f34-9cc7-c4983400b103
Abouhamzeh, Morteza
135fce39-e721-4cb1-a098-2b5bf30f820b
Elham, Ali
676043c6-547a-4081-8521-1567885ad41a
Ma, Yiyuan
ccea8698-10f9-4f34-9cc7-c4983400b103
Abouhamzeh, Morteza
135fce39-e721-4cb1-a098-2b5bf30f820b
Elham, Ali
676043c6-547a-4081-8521-1567885ad41a
Ma, Yiyuan, Abouhamzeh, Morteza and Elham, Ali
(2023)
Investigating aileron design for ultra-high aspect ratio wings.
In AIAA SCITECH 2023 Forum.
American Institute of Aeronautics and Astronautics..
(doi:10.2514/6.2023-2102).
Record type:
Conference or Workshop Item
(Paper)
Abstract
The Strut-Braced Wing (SBW) is a promising configuration for achieving next-generation sustainable and fuel-efficient aviation goals by using a composite Ultra-High Aspect Ratio Wing (UHARW) design. UHARW is more flexible than conventional wings, so the aileron effectiveness is a key constraint in the design and optimization of UHARW to avoid aileron reversal. This paper presents an aileron design methodology for UAHRW design and optimization by integrating the aileron’s required roll moment into a coupled adjoint aerostructural optimization tool for the aeroelastic and aerostructural investigations of the SBW configuration. The aeroelastic optimization results show that it is necessary to take into account aileron design variables in aeroelastic optimization as the wing structural weight can be reduced further. The aerostructural optimization results show a significant performance improvement of the SBW aircraft with considering the aileron design variables. The optimized SBW with two ailerons has significantly lower fuel weight and MTOW than the optimized SBW with only one aileron design. For both cases, the optimizer significantly reduces the wing drag by weakening/removing shock waves.
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e-pub ahead of print date: 19 January 2023
Venue - Dates:
AIAA SciTech 2023 Forum, Gaylord National Resort & Convention Center, National Harbor, United States, 2023-01-23 - 2023-01-27
Identifiers
Local EPrints ID: 484916
URI: http://eprints.soton.ac.uk/id/eprint/484916
PURE UUID: dc2ff230-88eb-4cd3-a001-f1e50881b640
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Date deposited: 24 Nov 2023 17:38
Last modified: 17 Mar 2024 06:00
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Author:
Yiyuan Ma
Author:
Morteza Abouhamzeh
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