Challenges and prospects of numerical optimization design for large civil aircraft aerodynamic shape

被引：0
作者：
Zhou Z. [1 ]
Huang J. [1 ]
Gao Z. [2 ]
Huang Y. [1 ]
Chen Z. [1 ]
Yu J. [1 ]
机构：
[1] Computational Aerodynamics Institute, China Aerodynamics Research and Development Center, Mianyang
[2] School of Aeronautics, Northwestern Polytechnical University, Xi'an
来源：
Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica | 2019年 / 40卷 / 01期
基金：
中国国家自然科学基金;
关键词：
Aero-structural optimization; Aerodynamic/sonic boom optimization; Coupled adjoint system; Integrated optimization system; Multidisciplinary optimization;
D O I：
10.7527/S1000-6893.2018.22370
中图分类号：
学科分类号：
摘要：
A systematic review of major aspects of aerodynamic shape optimization is carried out, summarizing the progress in all aspects of system optimization, including the discipline analysis, parametric method, grid deformation technology, sensitivity analysis, optimization algorithm, surrogate model, objective function/constraint processing, basic subjects and challenges of aerodynamic optimization. Combined with the research works carried out by our research team on the construction of optimization system, this paper addresses the requirement of the integrated design of the aerodynamic configuration of civil aircraft, summarizing the specific requirements of engineering type for constructing an optimized system. Prospects and suggestions for future research are also illustrated. Through the systematic discussion of the article, we hope to provide some meaningful suggestions and references for the researchers of designing aerodynamic numerical optimization, promoting the development of design aerodynamics and multidisciplinary optimization technology. © 2019, Press of Chinese Journal of Aeronautics. All right reserved.
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[1]  
Martins J.R.R.A., A coupled-adjoint method for high-fidelity. Aero-Structural optimization, pp. 79-87, (2002)
[2]  
Mader C.A., Kenway G.K.W., Martins J.R.R.A., Towards high-fidelity aerostructural optimization using a coupled adjoint approach: AIAA-2008-5968, (2008)
[3]  
Leoviriyakit K., Jameson A., Case studies in aero-structural wing planform and section optimization: AIAA-2004-5372, (2004)
[4]  
Mohammd A.Z., Brezillon J., Shape optimization using the aerostructural coupled adjoint approach for viscous flows, Proceedings of Evolutionary and Deterministic for Design, Optimization and Control, (2011)
[5]  
Marcelet M., Peter J., Carrier G., Sensitivity analysis of a strongly coupled aero-structural system using direct and adjoint methods: AIAA-2008-5863, (2008)
[6]  
Ghazlane I., Carrier G., Dumont A., Et al., Aerostructural adjoint method for flexible wing optimization: AIAA-2012-1924, (2012)
[7]  
Bai J.Q., Sun Z.W., Dong J.H., Et al., After body aerodynamic optimization design of transport airplane considering wing wake flow, Acta Aerodynamica Sinica, 33, 1, pp. 134-141, (2015)
[8]  
Wang C., Gao Z.H., Refined aerodynamic design optimization of a wing with small aspect ratio, Scientia Sinica Technologica, 45, 6, pp. 643-653, (2015)
[9]  
Li B., Deng Y.Q., Tang J., Et al., Discrete adjoint optimization method for 3D unstructured grid, Acta Aeronauticaet Astronautica Sinica, 35, 3, pp. 674-686, (2014)
[10]  
Zuo Y.T., Gao Z.H., Zhan H., Aerodynamic design method based on N-S equations and discrete adjoint approach, Acta Aerodynamica Sinica, 27, 1, pp. 67-72, (2009)
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