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地 面 颤 振 模 拟 试 验 技 术 研 究 进 展

  • Guiwei Zhang
  • , Zhaoqing Liu
  • , Lei Zhu
  • , Heng Zhang
  • , Wei Tian
  • , Weiguang Li
  • , Zhichun Yang
  • Northwestern Polytechnical University Xian
  • CAS - Xi'an Institute of Optics and Precision Mechanics
  • National Key Laboratory of Strength and Structural Integrity

科研成果: 期刊稿件文献综述同行评审

3 引用 (Scopus)

摘要

Flutter is a kind of aeroelastic dynamic stability problem that should be avoided during flight and may lead to disastrous consequences. Ground Flutter Simulation Test(GFST)is an emerging method for flutter testing,which directly uses the prototype structure or model structure of the aircraft as the test object and is a semi-physical simulation test technique. Aerodynamic simulation loading devices,such as shakers,are used to simulate the distributed aerodynamic loads on the structure,so that the aeroelastic stability characteristics of the real structure can be obtained on the ground(outside the wind tunnel). In this paper,the research status of GFST technology is analyzed from three aspects:reduced-order real-time reconstruction of the unsteady aerodynamic,unsteady aerodynamic simulation loading,and implementation of GFST. Future development directions of the GFST technology are also discussed.

投稿的翻译标题Research progress of ground flutter simulation test technology
源语言繁体中文
文章编号029229
期刊Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica
45
10
DOI
出版状态已出版 - 25 5月 2024

关键词

  • aerodynamic equivalence theory
  • excitation force control
  • ground flutter simulation test
  • loading system modeling
  • reduced-order real-time reconstruction of unsteady aerodynamic force

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