Abstract

In the approach of metric-based geometric parameterization, the concept of database filtration and proper orthogonal decomposition manipulation quantitatively enhances the generation of new geometric parameters so that the problem-oriented information is reflected in aerodynamic design. Compared with the conventional approach that applies only geometric filtration, this paper incorporates performance filtration so that the problem-oriented information is no longer limited to geometric constraints, thereby enabling the guidance of optimization direction in a more informed manner. This paper focuses on the pressure distribution of samples and their relationship with geometric variations. A variational autoencoder is employed to extract the dominant features of the aerodynamic potentials that an initial geometry can attain in optimization. The authors believe that the aerodynamic potential is reflected in how the pressure distribution differs from that of the initial geometry. Then, samples have to meet the performance filtration criterion based on pressure distribution proposed by designers according to their aerodynamic understanding of the optimization problem. Finally, the remaining collection of qualified samples generates new geometric parameters via proper orthogonal decomposition. The conventional and new approaches were validated in a two-dimensional airfoil case of drag coefficient optimization; the lift-to-drag ratio improved by 17.07% using the traditional method, and by 38.20% using the new approach. The pressure distribution shows that the performance filtration approach produces more supercritical properties than the geometric filtration approach. This implies that the performance filtration approach can capture more intricate details related to the aerodynamic performance of the airfoil.

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Data Availability Statement

Some or all data, models, or code that support the findings of this study are available from the corresponding author upon reasonable request.

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Go to Journal of Aerospace Engineering
Journal of Aerospace Engineering
Volume 37Issue 4July 2024

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Received: Oct 28, 2022
Accepted: Dec 6, 2023
Published online: Apr 24, 2024
Published in print: Jul 1, 2024
Discussion open until: Sep 24, 2024

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Ph.D. Candidate, Dept. of Aeronautics and Astronautics, Fudan Univ., No. 220 Handan Rd., Shanghai 200433, PR China. ORCID: https://orcid.org/0000-0001-6710-7556. Email: [email protected]
Shuyue Wang, Ph.D. [email protected]
GenAI Researcher, PilotD Automotive, No. 477 Zhengli Rd., Shanghai 200433, PR China. Email: [email protected]
Ph.D. Candidate, Dept. of Aeronautics and Astronautics, Fudan Univ., No. 220 Handan Rd., Shanghai 200433, PR China. Email: [email protected]
Zizhao Yuan [email protected]
Ph.D. Candidate, Dept. of Aeronautics and Astronautics, Fudan Univ., No. 220 Handan Rd., Shanghai 200433, PR China. Email: [email protected]
Yingjie Yang [email protected]
Master’s Student, Dept. of Aeronautics and Astronautics, Fudan Univ., No. 220 Handan Rd., Shanghai 200433, PR China. Email: [email protected]
Professor, Dept. of Aeronautics and Astronautics, Fudan Univ., No. 220 Handan Rd., Shanghai 200433, PR China (corresponding author). ORCID: https://orcid.org/0000-0003-4827-103X. Email: [email protected]

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