Low-Speed Flutter Wind Tunnel Experiment Technology Based on Binocular Vision System

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

Abstract

The low-speed flutter wind tunnel model of the wing is designed according to the structural dynamic similarity, integrated manufacturing of wing boxes, load-bearing ribs, skins and leading and trailing edges. The structural strength of the model meets the allowable strength requirements of the material. The binocular vision system is used to complete the flutter characteristic experiment of the wing model, and the expected result is achieved.

Original languageEnglish
Title of host publication2024 7th International Conference on Information Communication and Signal Processing, ICICSP 2024
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages444-448
Number of pages5
ISBN (Electronic)9798350355895
DOIs
StatePublished - 2024
Event7th International Conference on Information Communication and Signal Processing, ICICSP 2024 - Zhoushan, China
Duration: 21 Sep 202423 Sep 2024

Publication series

Name2024 7th International Conference on Information Communication and Signal Processing, ICICSP 2024

Conference

Conference7th International Conference on Information Communication and Signal Processing, ICICSP 2024
Country/TerritoryChina
CityZhoushan
Period21/09/2423/09/24

Keywords

  • Binocular vision
  • Flutter
  • Integration
  • Wind tunnel experiment
  • Wing model

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