Please use this identifier to cite or link to this item: https://hdl.handle.net/20.500.11851/10995
Title: Design of the ONERA M6 wing by shape optimization under uncertainty
Other Titles: ONERA M6 kanadının belirsizlik altında şekil optimizasyonu ile tasarımı
Authors: Demir, G.
Görgülüarslan, R.M.
Aradağ, S.
Keywords: Computational fluid dynamics; proper orthogonal decomposition; robust optimization; uncertainty
Aerodynamics; Computational fluid dynamics; Decomposition methods; Orthogonal functions; Principal component analysis; Radial basis function networks; Wings; Design Exploration; Design variables; Exploration methods; Optimization techniques; Orthogonal decomposition; Proper Orthogonal; Proper orthogonal decomposition; Robust optimization; Shape-optimization; Uncertainty; Shape optimization
Issue Date: 2024
Publisher: Gazi Universitesi
Abstract: Aerodynamic shape optimization processes are often used for complex problems that meet single or multi-objective design requirements. The robust aerodynamic shape optimization techniques with a high number of design variables that consider uncertainties have a huge computational burden compared to the traditional aerodynamic shape optimization techniques without considering uncertainties. To overcome this issue, in this study, the proper orthogonal decomposition is integrated with the inductive design exploration method to use for the robust shape optimization of the ONERA M6 wing. The proper orthogonal decomposition method is utilized for reducing the number of design variables of the wing geometry. The cost due to the computational fluid dynamics analysis is mitigated by incorporating the proper orthogonal decomposition with a surrogate modeling technique called the radial basis function. The robust optimization is conducted by the proposed approach based on the inductive design exploration method by accounting for uncertainties of the Mach number in the transonic flow regime. The agreement between the performance predictions of the robust designs and the computational fluid dynamics analysis results showed the effectiveness of the proposed approach. © 2024 Gazi Universitesi Muhendislik-Mimarlik. All rights reserved.
URI: https://doi.org/10.17341/gazimmfd.1190263
https://hdl.handle.net/20.500.11851/10995
ISSN: 1300-1884
Appears in Collections:Scopus İndeksli Yayınlar Koleksiyonu / Scopus Indexed Publications Collection

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