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2024 | OriginalPaper | Chapter

3. Progress of ARI_OPT Software for Aerodynamic Shape Optimization

Authors : Chuang Wei, Zhansen Qian, Long Yang

Published in: Advanced Computational Methods and Design for Greener Aviation

Publisher: Springer International Publishing

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Abstract

In order to improve the design efficiency and design effect of the aerodynamic shape of the aircraft, the aerodynamic optimization design tool ARI_OPT was developed based on the numerical optimization design technology. ARI_OPT includes modules such as aerodynamic shape parameterization, grid automatic generation, surrogate model optimization, multi-level numerical simulation, and high-efficiency optimization algorithm. The basic principles, methods and verification results of each module are briefly introduced. The functional verification results of numerical function cases and the application results of typical single-objective and multi-objective aerodynamic shape optimization problems such as airfoil, multi-element airfoil and wing-body by ARI_OPT, which strongly prove its effectiveness.

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Literature
1.
go back to reference Peigin S, Zhu ZQ, Epstein B (2014) Applicable numerical optimization methods for aerodynamic design of civil aircraft. Acta Aeronautica et Astronautica Sinica 35(1):58–69 Peigin S, Zhu ZQ, Epstein B (2014) Applicable numerical optimization methods for aerodynamic design of civil aircraft. Acta Aeronautica et Astronautica Sinica 35(1):58–69
2.
go back to reference Zhou Z, Huang JT, Gao ZH, Huang Y, Chen ZB, Yu J (2019) Challenges and prospects of numerical optimization design for large civil aircraft aerodynamic shape. Acta Aeronautica et Astronautica Sinica 40(1):69–90CrossRef Zhou Z, Huang JT, Gao ZH, Huang Y, Chen ZB, Yu J (2019) Challenges and prospects of numerical optimization design for large civil aircraft aerodynamic shape. Acta Aeronautica et Astronautica Sinica 40(1):69–90CrossRef
3.
go back to reference Han ZH, Zhang Y, Xu CZ, Wang K, Wu MM, Zhu Z, Song WP (2019) Aerodynamic optimization design of large civil aircraft wings using surrogate-based model. Acta Aeronautica et Astronautica Sinica 40(1):155–170 Han ZH, Zhang Y, Xu CZ, Wang K, Wu MM, Zhu Z, Song WP (2019) Aerodynamic optimization design of large civil aircraft wings using surrogate-based model. Acta Aeronautica et Astronautica Sinica 40(1):155–170
4.
go back to reference Shankaran S, Jameson A, Martinelli I (2008) Continuous adjoint method for unstructured grids. AIAA J 46(5):226–239 Shankaran S, Jameson A, Martinelli I (2008) Continuous adjoint method for unstructured grids. AIAA J 46(5):226–239
5.
go back to reference Palacios F, Economon TD, Aranake AC (2014) Stanford University Unstructured (SU2): open-source analysis and design technology for turbulent flows. In: AIAA science and technology forum and exposition 2014: 52nd aerospace sciences meeting, National Harbor, MD, 13–17 Jan 2014 Palacios F, Economon TD, Aranake AC (2014) Stanford University Unstructured (SU2): open-source analysis and design technology for turbulent flows. In: AIAA science and technology forum and exposition 2014: 52nd aerospace sciences meeting, National Harbor, MD, 13–17 Jan 2014
6.
go back to reference LeDoux ST, Herling WW, Fatta GJ (2004) MDOPT-A multidisciplinary design optimization system using higher order analysis. In: 10th AIAA/ISSMO multidisciplinary analysis and optimization conference LeDoux ST, Herling WW, Fatta GJ (2004) MDOPT-A multidisciplinary design optimization system using higher order analysis. In: 10th AIAA/ISSMO multidisciplinary analysis and optimization conference
7.
go back to reference Nielsen EJ, Diskin B, Yamaleev NK (2010) Discrete adjoint-based design optimization of unsteady turbulent flows on dynamic unstructured grids. AIAA J 48(6):1195–1206CrossRef Nielsen EJ, Diskin B, Yamaleev NK (2010) Discrete adjoint-based design optimization of unsteady turbulent flows on dynamic unstructured grids. AIAA J 48(6):1195–1206CrossRef
8.
go back to reference Park M (2011) Low boom configuration analysis with FUN3D adjoint simulation framework. In: 29th AIAA applied aerodynamics conference Park M (2011) Low boom configuration analysis with FUN3D adjoint simulation framework. In: 29th AIAA applied aerodynamics conference
9.
go back to reference Brezillon J, Dwight RP (2009) Aerodynamic shape optimization using the discrete adjoint of the Navier-Stokes equations: applications towards complex 3D configurations. In: CEAS/KATnet II conference on key aerodynamic technologies, Bremen Germany. machtWissen Brezillon J, Dwight RP (2009) Aerodynamic shape optimization using the discrete adjoint of the Navier-Stokes equations: applications towards complex 3D configurations. In: CEAS/KATnet II conference on key aerodynamic technologies, Bremen Germany. machtWissen
10.
go back to reference Widhalm M, Ronzheimer A, Hepperle M (2009) Comparison between gradient-free and adjoint based aerodynamic optimization of a flying wing transport aircraft in the preliminary design. In: 25th AIAA applied aerodynamics conference Widhalm M, Ronzheimer A, Hepperle M (2009) Comparison between gradient-free and adjoint based aerodynamic optimization of a flying wing transport aircraft in the preliminary design. In: 25th AIAA applied aerodynamics conference
11.
go back to reference Carrier G, Destarac D, Dumont A, Meheut M, Salah EI Din I, Peter J, Saloua I, Ben Khelil S, Brezillon J, Pestana M (2014) Gradient-based aerodynamic optimization with the elsA software. In: 52th Aerospace sciences meeting Carrier G, Destarac D, Dumont A, Meheut M, Salah EI Din I, Peter J, Saloua I, Ben Khelil S, Brezillon J, Pestana M (2014) Gradient-based aerodynamic optimization with the elsA software. In: 52th Aerospace sciences meeting
12.
go back to reference Dumont A, Le Pape A, Peter J, Huberson S (2011) Aerodynamic shape optimization of hovering rotors using a discrete adjoint of the Reynolds-averaged Navier-Stokes equations. J Am Helicopter Soc 56(3):1–11CrossRef Dumont A, Le Pape A, Peter J, Huberson S (2011) Aerodynamic shape optimization of hovering rotors using a discrete adjoint of the Reynolds-averaged Navier-Stokes equations. J Am Helicopter Soc 56(3):1–11CrossRef
13.
go back to reference Huang JT, Zhou Z, Gao ZH (2017) Aerodynamic multi-objective integrated optimization based on principal component analysis. Chin J Aeronaut 30(4):1336–1348CrossRef Huang JT, Zhou Z, Gao ZH (2017) Aerodynamic multi-objective integrated optimization based on principal component analysis. Chin J Aeronaut 30(4):1336–1348CrossRef
14.
go back to reference Li J, Gao ZH, Zhao K (2015) Robust design of transonic laminar wing-body configuration based on direct manipulated FFD technique. Scientia Sinica Technologica 46(9):964–974 Li J, Gao ZH, Zhao K (2015) Robust design of transonic laminar wing-body configuration based on direct manipulated FFD technique. Scientia Sinica Technologica 46(9):964–974
15.
go back to reference Bai JQ, Lei RW, Yang TH, Wang H, He XL, Qiu YS (2019) Progress of adjoint-based aerodynamic optimization design for large civil aircraft. Acta Aeronautica et Astronautica Sinica 40(1):103–120 Bai JQ, Lei RW, Yang TH, Wang H, He XL, Qiu YS (2019) Progress of adjoint-based aerodynamic optimization design for large civil aircraft. Acta Aeronautica et Astronautica Sinica 40(1):103–120
16.
go back to reference Han ZH (2016) Kriging surrogate model and its application to design optimization: a review of recent progress. Acta Aeronautics et Astronautica Sinica 37(11):3197–3225MathSciNet Han ZH (2016) Kriging surrogate model and its application to design optimization: a review of recent progress. Acta Aeronautics et Astronautica Sinica 37(11):3197–3225MathSciNet
17.
go back to reference Zhao T, Zhang YF, Chen HX, Chen YC, Zhang M (2015) Aerodynamics optimization method of supercritical airfoil geared to the performance of swept and tapered wing. Scientia Sinica Technologica 45(10):89–101 Zhao T, Zhang YF, Chen HX, Chen YC, Zhang M (2015) Aerodynamics optimization method of supercritical airfoil geared to the performance of swept and tapered wing. Scientia Sinica Technologica 45(10):89–101
18.
go back to reference Zhao QJ, Zhang W, Yuan X, Zhu Z, Wang B (2019) Optimization design of coaxial rotor aerodynamic planform. J Nanjing Univ Aeronaut Astronaut 51(2):160–165 Zhao QJ, Zhang W, Yuan X, Zhu Z, Wang B (2019) Optimization design of coaxial rotor aerodynamic planform. J Nanjing Univ Aeronaut Astronaut 51(2):160–165
19.
go back to reference Tang Z, Huang M (2001) Control theory based airfoil design using Euler equations. Acta Aerodynamica Sinica 19(3):262–270 Tang Z, Huang M (2001) Control theory based airfoil design using Euler equations. Acta Aerodynamica Sinica 19(3):262–270
20.
go back to reference Wei C, Zhang TJ, Liu TZ (2017) Multi-objective optimization of fowler flap on general aircraft. Acta Aerodynamica Sinica 35(4):572–578 Wei C, Zhang TJ, Liu TZ (2017) Multi-objective optimization of fowler flap on general aircraft. Acta Aerodynamica Sinica 35(4):572–578
21.
go back to reference Kulfan BM, Bussoletti JE (2006) Low boom configuration analysis with FUN3D adjoint simulation framework. In: AIAA/ISSMO multidisciplinary analysis and optimization conference, Portsmouth, Virginia, AIAA paper 2006-6948 Kulfan BM, Bussoletti JE (2006) Low boom configuration analysis with FUN3D adjoint simulation framework. In: AIAA/ISSMO multidisciplinary analysis and optimization conference, Portsmouth, Virginia, AIAA paper 2006-6948
22.
go back to reference Hicks RM, Henne PA (1978) Wing design by numerical optimization. J Aircr 15(7):407–412 Hicks RM, Henne PA (1978) Wing design by numerical optimization. J Aircr 15(7):407–412
23.
go back to reference Sederberg TW, Parry SR (1986) Free-form deformation of solid geometric models. In: Proceedings of the 13th annual conference on computer graphics and interactive techniques Sederberg TW, Parry SR (1986) Free-form deformation of solid geometric models. In: Proceedings of the 13th annual conference on computer graphics and interactive techniques
24.
go back to reference De Boer A, Van der Schoot MS, Bijl H (2007) Mesh deformation based on radial basis function interpolation. Comput Struct 85(11–13):784–795 De Boer A, Van der Schoot MS, Bijl H (2007) Mesh deformation based on radial basis function interpolation. Comput Struct 85(11–13):784–795
Metadata
Title
Progress of ARI_OPT Software for Aerodynamic Shape Optimization
Authors
Chuang Wei
Zhansen Qian
Long Yang
Copyright Year
2024
DOI
https://doi.org/10.1007/978-3-031-61109-4_3

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