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Removing mass loading effects of multi-transducers using Sherman-Morrison-Woodbury formula in modal test

  • Published:2019-10 Issue: Volume:93 Page:105241
  • ISSN:1270-9638
  • Container-title:Aerospace Science and Technology
  • language:en
  • Short-container-title:Aerospace Science and Technology

Author:

Zhu Rui,Fei Qingguo,Jiang Dong,Cao Zhifu

Funder

National Natural Science Foundation of China

Jiangsu Natural Science Foundation

Postgraduate Research & Practice Innovation Program of Jiangsu Province

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference23 articles.

1. Nonstationary random vibration analysis of wing with geometric nonlinearity under correlated excitation;Li;J. Aircr.,2018

2. Monitoring multi-axial vibrations of flexible rockets using sensor-instrumented reference strain structures;Tsushima;Aerosp. Sci. Technol.,2017

3. Modal energy analysis for mechanical systems excited by spatially correlated loads;Zhang;Mech. Syst. Signal Process.,2018

4. A study on adaptive vibration control and energy conversion of highly flexible multifunctional wings;Tsushima;Aerosp. Sci. Technol.,2018

5. Improving the reliability of the frequency response function through semi-direct finite element model updating;Lim;Aerosp. Sci. Technol.,2016

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