Flying qualities reliability constraints in aircraft conceptual design using time-marching simulations
Flying qualities reliability constraints in aircraft conceptual design using time-marching simulations
Aircraft conceptual design, especially when novel concepts are involved, is inherently affected by uncertainty. Although many efforts are done to include more physics at the earliest design phases, often information on impact of the underlying uncertainty is missing. This work proposes an approach to incorporate uncertainty into aircraft conceptual design through reliability constraints on some desired dynamic performance requirements. These are estimated from unsteady time-domain simulations through a system identification process, leveraging on three available aerodynamic fidelity levels. Uncertainty propagation is addressed by a polynomial chaos expansion technique. After presenting the structure and the validation of the proposed framework, a demonstrative application of fuel mass optimization for a transport aircraft under uncertainty is performed, with reliability constraints on short period characteristics.
American Institute of Aeronautics and Astronautics
Saporito, Marco
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Da Ronch, Andrea
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Bartoli, Nathalie
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Defoort, Sébastien
67f3e4ca-1184-4d5a-b380-b69ef27c5fd0
Saporito, Marco
13c1def8-ba40-4f5e-9a0a-6cf7f60e1063
Da Ronch, Andrea
a2f36b97-b881-44e9-8a78-dd76fdf82f1a
Bartoli, Nathalie
2cfac8e2-24a5-4516-9f0f-33beae42adb2
Defoort, Sébastien
67f3e4ca-1184-4d5a-b380-b69ef27c5fd0
Saporito, Marco, Da Ronch, Andrea, Bartoli, Nathalie and Defoort, Sébastien
(2021)
Flying qualities reliability constraints in aircraft conceptual design using time-marching simulations.
In Proceedings of the American Institute of Aeronautics and Astronautics (AIAA) 2021.
American Institute of Aeronautics and Astronautics..
(doi:10.2514/6.2021-3101).
Record type:
Conference or Workshop Item
(Paper)
Abstract
Aircraft conceptual design, especially when novel concepts are involved, is inherently affected by uncertainty. Although many efforts are done to include more physics at the earliest design phases, often information on impact of the underlying uncertainty is missing. This work proposes an approach to incorporate uncertainty into aircraft conceptual design through reliability constraints on some desired dynamic performance requirements. These are estimated from unsteady time-domain simulations through a system identification process, leveraging on three available aerodynamic fidelity levels. Uncertainty propagation is addressed by a polynomial chaos expansion technique. After presenting the structure and the validation of the proposed framework, a demonstrative application of fuel mass optimization for a transport aircraft under uncertainty is performed, with reliability constraints on short period characteristics.
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e-pub ahead of print date: 28 July 2021
Venue - Dates:
AIAA AVIATION 2021 FORUM, 2021-08-02 - 2021-08-06
Identifiers
Local EPrints ID: 478012
URI: http://eprints.soton.ac.uk/id/eprint/478012
PURE UUID: b8b9797c-2476-4fca-bcb7-2e88eba77d20
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Date deposited: 19 Jun 2023 16:56
Last modified: 17 Mar 2024 03:32
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Author:
Marco Saporito
Author:
Nathalie Bartoli
Author:
Sébastien Defoort
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