先进战斗机气动弹性设计综述

doi:10.7527/S1000-6893.2019.23430

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先进战斗机气动弹性设计综述

李秋彦, 李刚, 魏洋天, 冉玉国, 吴波, 谭光辉, 李焱, 陈识, 雷博淇, 徐钦炜

中国航空工业成都飞机设计研究所, 成都 610091

收稿日期:2019-09-02 修回日期:2019-09-27 出版日期:2020-06-15 发布日期:2019-11-07
通讯作者: 李秋彦 E-mail:li-qiuyan@163.com

Review of aeroelasticity design for advanced fighter

LI Qiuyan, LI Gang, WEI Yangtian, RAN Yuguo, WU Bo, TAN Guanghui, LI Yan, CHEN Shi, LEI Boqi, XU Qinwei

AVIC Chengdu Aircraft Design and Research Institute, Chengdu 610091, China

Received:2019-09-02 Revised:2019-09-27 Online:2020-06-15 Published:2019-11-07

摘要/Abstract

摘要： 中国新一代战斗机的研发引领了飞机设计领域各项技术的创新和发展。针对研制总要求和任务特殊性，中国航空工业成都飞机设计研究所气动弹性专业建立了精益气动弹性设计与验证技术体系。基于多学科优化设计流程，开展了旨在提高飞机气动弹性品质的关键技术攻关、气弹优化设计和分析工作。完成了考虑含全动翼面结构非线性的全机动力学特性地面试验、亚跨超声速颤振模型风洞试验和气动弹性飞行试验验证。在较短的研发周期内，成功实现气动弹性设计目标，为新一代战斗机的成功研制提供了技术保障。描述了该飞机气动弹性设计历程、主要技术工作以及在此基础上取得的技术进步、能力提升以及具有研究所特色的气动弹性设计知识工程建设。

关键词: 战斗机, 气动弹性, 优化设计, 地面试验, 飞行试验, 颤振风洞模型, 气动伺服弹性, 知识工程

Abstract: The birth of Chinese new-generation fighter leads all the technical innovation and development in aircraft designing field. Lean aero-elasticity design and verification technology system were established in AVIC Chengdu Aircraft Design and Research Institute according to the project development requirements and task particularity. Critical technology research and optimization design and analysis aiming at enhancing aircraft aero-elastic quality were carried out based on multi-disciplinary design optimization process. Whole aircraft dynamic characteristics ground test with consideration of all-movable surface structural nonlinearity, subsonic/transonic/supersonic flutter model wind tunnel tests that cover all Mach numbers and flight aero-elasticity test verification were completed and passed. Aero-elasticity design objective was achieved within a short development period, providing technical support for successful development of new-generation fighter. This paper describes the design process, major technical work of the aircraft, as well as the gained technical progress, capability enhancement, and knowledge engineering construction of aeroelastic design with research institute characteristics.

Key words: fighter, aeroelasticity, optimization design, ground test, flight test, flutter wind tunnel model, aeroservoelasticity, knowledge engineering

中图分类号:

V211.47

李秋彦, 李刚, 魏洋天, 冉玉国, 吴波, 谭光辉, 李焱, 陈识, 雷博淇, 徐钦炜. 先进战斗机气动弹性设计综述[J]. 航空学报, 2020, 41(6): 523430-523430.

LI Qiuyan, LI Gang, WEI Yangtian, RAN Yuguo, WU Bo, TAN Guanghui, LI Yan, CHEN Shi, LEI Boqi, XU Qinwei. Review of aeroelasticity design for advanced fighter[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2020, 41(6): 523430-523430.

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先进战斗机气动弹性设计综述

Review of aeroelasticity design for advanced fighter

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