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Deep–learning framework for aircraft aerodynamics prediction

Deep–learning framework for aircraft aerodynamics prediction
Deep–learning framework for aircraft aerodynamics prediction
The present paper aims to develop a deep--learning framework able to predict distributed quantities of aircrafts flying in transonic regime, which are critical for the determination of aerodynamic loads and aeroelastic analysis. Angle of attack and Mach number are chosen as the two independent parameters for the reduced--order models. A comparative assessment of the proposed non--linear model is made with Proper Orthogonal Decomposition approach in order to highlight strengths and weaknesses of each method. The accuracy of the data--driven machine--learning method in modelling steady--state aerodynamics is assessed with three benchmark cases of 3D--wings in transonic regime. Despite the challenges of the analyzed scenarios, promising results are obtained for each test case, showing the effectiveness of the model implemented.
Aerospace Research Central
Immordino, Gabriele
ed9626cc-aa2b-40be-b376-0868967e5e65
Da Ronch, Andrea
a2f36b97-b881-44e9-8a78-dd76fdf82f1a
Righi, Marcello
26caafe6-a86f-445b-82ca-9789ae4109ca
Immordino, Gabriele
ed9626cc-aa2b-40be-b376-0868967e5e65
Da Ronch, Andrea
a2f36b97-b881-44e9-8a78-dd76fdf82f1a
Righi, Marcello
26caafe6-a86f-445b-82ca-9789ae4109ca

Immordino, Gabriele, Da Ronch, Andrea and Righi, Marcello (2023) Deep–learning framework for aircraft aerodynamics prediction. In AIAA AVIATION 2023 Forum. Aerospace Research Central.. (doi:10.2514/6.2023-3846).

Record type: Conference or Workshop Item (Paper)

Abstract

The present paper aims to develop a deep--learning framework able to predict distributed quantities of aircrafts flying in transonic regime, which are critical for the determination of aerodynamic loads and aeroelastic analysis. Angle of attack and Mach number are chosen as the two independent parameters for the reduced--order models. A comparative assessment of the proposed non--linear model is made with Proper Orthogonal Decomposition approach in order to highlight strengths and weaknesses of each method. The accuracy of the data--driven machine--learning method in modelling steady--state aerodynamics is assessed with three benchmark cases of 3D--wings in transonic regime. Despite the challenges of the analyzed scenarios, promising results are obtained for each test case, showing the effectiveness of the model implemented.

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More information

Accepted/In Press date: June 2023
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

Identifiers

Local EPrints ID: 484022
URI: http://eprints.soton.ac.uk/id/eprint/484022
PURE UUID: e87d3d41-ad83-40cf-8d59-cc033b0f8e16
ORCID for Andrea Da Ronch: ORCID iD orcid.org/0000-0001-7428-6935

Catalogue record

Date deposited: 09 Nov 2023 17:32
Last modified: 18 Mar 2024 03:25

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Contributors

Author: Gabriele Immordino
Author: Andrea Da Ronch ORCID iD
Author: Marcello Righi

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