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ACTA AERONAUTICAET ASTRONAUTICA SINICA >

2020 , Vol. 41 >Issue 6: 523430 - 523430

DOI: https://doi.org/10.7527/S1000-6893.2019.23430

Review

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

Received date: 2019-09-02

  Revised date: 2019-09-27

  Online published: 2019-11-07

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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

Cite this article

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 . DOI: 10.7527/S1000-6893.2019.23430

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