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Flying qualities reliability constraints in aircraft conceptual design using time-marching simulations

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
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
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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More information

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
ORCID for Marco Saporito: ORCID iD orcid.org/0000-0003-1975-2811
ORCID for Andrea Da Ronch: ORCID iD orcid.org/0000-0001-7428-6935

Catalogue record

Date deposited: 19 Jun 2023 16:56
Last modified: 17 Mar 2024 03:32

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Contributors

Author: Marco Saporito ORCID iD
Author: Andrea Da Ronch ORCID iD
Author: Nathalie Bartoli
Author: Sébastien Defoort

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