Governed by: Ministry of Industry and Information Technology of the People's Republic of China
Sponsored by: Northwestern Polytechnical University  Chinese Society Aeronautics and Astronautics
Address: Aviation Building,Youyi Campus, Northwestern Polytechnical University
Wet Modal analysis and experiment research of flexible airship envelop
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China Special Aircraft Research Institute,Test and Metrology Center,Jingmen,448035 China

Clc Number:

V214.3

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    Abstract:

    In order to research the influence of the flow field around the large-scale flexible airship on its modal performance, the air around the airship was assumed as compressible potential fluid, the influence of air with structure vibration is considered as additional mass was added to the capsule structure. The modal test of the internal pressure of the 1:60 main airbag at 2kpa、4kpa、6kpa、8kpa and 10kpa was completed, the virbrometer based on the principle of laser vibration measurement was applied to measure the first three modes of the main airbag. Also the wet modal analysis method based on the additional mass was used to analyze the first 3 modes of the main airbag under 5 different internal pressure. The test and calculation results prove that the wet modal analysis method on the additional mass can be used for modal analysis for large flexible structure.

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LIU Lu, Zhang Wei, Wang Pengfei. Wet Modal analysis and experiment research of flexible airship envelop[J]. Advances in Aeronautical Science and Engineering,2022,13(4):162-167

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History
  • Received:July 22,2021
  • Revised:January 27,2022
  • Adopted:February 26,2022
  • Online: June 08,2022
  • Published: