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SDF-GAN: aerofoil shape parameterisation via an adversarial auto-encoder

SDF-GAN: aerofoil shape parameterisation via an adversarial auto-encoder
SDF-GAN: aerofoil shape parameterisation via an adversarial auto-encoder
Current aerodynamic design processes suffer from expensive optimisation procedures, in part due to the requirement to search large design spaces. Recent advances in deep learning, and more precisely the development of high quality generative models such as Generative Adversarial Networks (GANs) and Variational Auto-Encoders (VAEs), have opened up new possibilities for shape parameterisation and aerodynamic design. As the focus of work in this area so far has primarily been on generative aerofoil design via coordinate-based shape representations,aerofoil generation via image-based shape representation is yet to receive much attention. This study aims to rectify this by investigating aerofoil shape generation using signed distance field geometry representations. A key issue with direct geometry representation is the potential lack of smoothness in the output design. Two features are proposed to mitigate this: the first is an auto-encoding architecture, which was found to help drive the output designs to smoother geometries; the second is a Hanning filter provided by XFOIL, which acts to smooth the surface speed distribution and return the corresponding geometry. Network hyper-parameters are set through an optimisation procedure using an LP-tau design of experiments. The approach is compared to alternative state-of-the-art parameterisation techniques.
Bamford, Joshua Thomas
e8cdc100-0e20-475c-8d67-01b191711526
Keane, Andy
26d7fa33-5415-4910-89d8-fb3620413def
Toal, David
dc67543d-69d2-4f27-a469-42195fa31a68
Bamford, Joshua Thomas
e8cdc100-0e20-475c-8d67-01b191711526
Keane, Andy
26d7fa33-5415-4910-89d8-fb3620413def
Toal, David
dc67543d-69d2-4f27-a469-42195fa31a68

Bamford, Joshua Thomas, Keane, Andy and Toal, David (2024) SDF-GAN: aerofoil shape parameterisation via an adversarial auto-encoder. 2024 AIAA AVIATION Forum, Caesars Forum, Las Vegas, United States. 29 Jul - 02 Aug 2024. 23 pp .

Record type: Conference or Workshop Item (Paper)

Abstract

Current aerodynamic design processes suffer from expensive optimisation procedures, in part due to the requirement to search large design spaces. Recent advances in deep learning, and more precisely the development of high quality generative models such as Generative Adversarial Networks (GANs) and Variational Auto-Encoders (VAEs), have opened up new possibilities for shape parameterisation and aerodynamic design. As the focus of work in this area so far has primarily been on generative aerofoil design via coordinate-based shape representations,aerofoil generation via image-based shape representation is yet to receive much attention. This study aims to rectify this by investigating aerofoil shape generation using signed distance field geometry representations. A key issue with direct geometry representation is the potential lack of smoothness in the output design. Two features are proposed to mitigate this: the first is an auto-encoding architecture, which was found to help drive the output designs to smoother geometries; the second is a Hanning filter provided by XFOIL, which acts to smooth the surface speed distribution and return the corresponding geometry. Network hyper-parameters are set through an optimisation procedure using an LP-tau design of experiments. The approach is compared to alternative state-of-the-art parameterisation techniques.

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Published date: 29 July 2024
Venue - Dates: 2024 AIAA AVIATION Forum, Caesars Forum, Las Vegas, United States, 2024-07-29 - 2024-08-02

Identifiers

Local EPrints ID: 490027
URI: http://eprints.soton.ac.uk/id/eprint/490027
PURE UUID: 671613d8-79d3-4b84-8c15-e814bd1c0925
ORCID for Joshua Thomas Bamford: ORCID iD orcid.org/0000-0001-7416-5703
ORCID for Andy Keane: ORCID iD orcid.org/0000-0001-7993-1569
ORCID for David Toal: ORCID iD orcid.org/0000-0002-2203-0302

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Date deposited: 13 May 2024 17:19
Last modified: 14 May 2024 01:59

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