High-fidelity aero-structural optimisation using individual discipline feasible strategy
High-fidelity aero-structural optimisation using individual discipline feasible strategy
Aero–structural optimisation is a challenging aspect of aircraft design. The state–of–the–art in this field proposes several different techniques, which can be classified by architecture of the algorithm. Choosing among them, mostly depends on the nature of the problem one wants to study and on how the coupling between Aerodynamics and Structures is carried out. The Individual Discipline Feasible (IDF) technique proposes a monolithic approach to the optimisation problem, where the different disciplines are optimised together in a unified framework, but without any direct coupling. This feature is of particular interest for those cases where an interface between the disciplinary analyses is hard to implement, or when it increases significantly the computational cost. However, to guarantee convergence to a physically feasible solution, additional constraints must be defined, and surrogate variables must be introduced. This paper presents an application of the IDF strategy to high–fidelity aero–structural optimisation of a concept tailplane design. With no relevant demonstrations in this area, our results are very promising and indicate an optimised solution is found in few iterations.
Aerospace Research Central
Conti, Claudio
6faac28b-c3e1-41a2-abb3-4a5469d9bace
Mandorino, Massimo
ebdcfe45-56f7-4edc-b3f2-bf15ff85d853
Da Ronch, Andrea
a2f36b97-b881-44e9-8a78-dd76fdf82f1a
Elham, Ali
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Conti, Claudio
6faac28b-c3e1-41a2-abb3-4a5469d9bace
Mandorino, Massimo
ebdcfe45-56f7-4edc-b3f2-bf15ff85d853
Da Ronch, Andrea
a2f36b97-b881-44e9-8a78-dd76fdf82f1a
Elham, Ali
676043c6-547a-4081-8521-1567885ad41a
Conti, Claudio, Mandorino, Massimo, Da Ronch, Andrea and Elham, Ali
(2023)
High-fidelity aero-structural optimisation using individual discipline feasible strategy.
In AIAA AVIATION 2023 Forum.
Aerospace Research Central..
(doi:10.2514/6.2023-3317).
Record type:
Conference or Workshop Item
(Paper)
Abstract
Aero–structural optimisation is a challenging aspect of aircraft design. The state–of–the–art in this field proposes several different techniques, which can be classified by architecture of the algorithm. Choosing among them, mostly depends on the nature of the problem one wants to study and on how the coupling between Aerodynamics and Structures is carried out. The Individual Discipline Feasible (IDF) technique proposes a monolithic approach to the optimisation problem, where the different disciplines are optimised together in a unified framework, but without any direct coupling. This feature is of particular interest for those cases where an interface between the disciplinary analyses is hard to implement, or when it increases significantly the computational cost. However, to guarantee convergence to a physically feasible solution, additional constraints must be defined, and surrogate variables must be introduced. This paper presents an application of the IDF strategy to high–fidelity aero–structural optimisation of a concept tailplane design. With no relevant demonstrations in this area, our results are very promising and indicate an optimised solution is found in few iterations.
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e-pub ahead of print date: 8 June 2023
Venue - Dates:
AIAA AVIATION 2023 Forum, , San Diego, United States, 2023-06-12 - 2023-06-16
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Local EPrints ID: 484078
URI: http://eprints.soton.ac.uk/id/eprint/484078
PURE UUID: f7d80191-2a09-4b02-8b06-896d64ccef8e
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Date deposited: 09 Nov 2023 18:13
Last modified: 18 Mar 2024 03:25
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Author:
Claudio Conti
Author:
Massimo Mandorino
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