民用飞机气动外形数值优化设计面临的挑战与展望

周铸; 黄江涛; 高正红; 黄勇; 陈作斌; 余婧

doi:10.7527/S1000-6893.2018.22370

航空学报 >

2019 , Vol. 40 >Issue 1: 522370 - 522370

DOI: https://doi.org/10.7527/S1000-6893.2018.22370

流体力学与飞行力学

民用飞机气动外形数值优化设计面临的挑战与展望

周铸 ,
黄江涛 ,
高正红 ,
黄勇 ,
陈作斌 ,
余婧

展开

1. 中国空气动力研究与发展中心计算空气动力研究所, 绵阳 621000;
2. 西北工业大学航空学院, 西安 710072

收稿日期: 2018-05-28

修回日期: 2018-06-20

网络出版日期: 2018-08-27

基金资助

国家自然科学基金（11402288）；国家重点研发计划（2016YFB0200704）

收起

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

ZHOU Zhu ,
HUANG Jiangtao ,
GAO Zhenghong ,
HUANG Yong ,
CHEN Zuobin ,
YU Jing

Expand

1. Computational Aerodynamics Institute, China Aerodynamics Research and Development Center, Mianyang 621000, China;
2. School of Aeronautics, Northwestern Polytechnical University, Xi'an 710072, China

Received date: 2018-05-28

Revised date: 2018-06-20

Online published: 2018-08-27

Supported by

National Natural Science Foundation of China (11402288); National Key Research and Development Program of China(2016YFB0200704)

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摘要

系统回顾了气动外形优化的主要环节，对优化体系中学科分析、参数化建模、网格重构技术、敏度分析、优化算法、代理模型、目标函数/约束处理等各个环节的进展，及气动综合优化面临的挑战、基础科学问题进行了总结。结合课题组在优化体系建设上开展的研究工作，针对民用飞机气动外形综合设计的需求，提炼了工程型号对优化体系构建的具体要求。并对今后的研究工作以及未来发展方向进行了展望与建议。通过文章系统整理论述，希望能够为气动数值优化设计研究人员提供一些有意义的建议和参考，促进设计空气动力学、以及多学科优化技术的发展。

关键词： 综合优化体系; 多学科优化; 耦合伴随系统; 气动/结构优化; 气动/声爆优化

本文引用格式

周铸 , 黄江涛 , 高正红 , 黄勇 , 陈作斌 , 余婧 . 民用飞机气动外形数值优化设计面临的挑战与展望[J]. 航空学报, 2019 , 40(1) : 522370 -522370 . DOI: 10.7527/S1000-6893.2018.22370

Abstract

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.

Key words： integrated optimization system; multidisciplinary optimization; coupled adjoint system; aero-structural optimization; aerodynamic/sonic boom optimization

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