Mathematical modeling and experimental study of damping behavior of a cantilever carbon fiber–reinforced polymer composite hollow member with metal inserts

Komal Chawla, Samit Ray-Chaudhuri

Research output: Contribution to journalArticlepeer-review

6 Scopus citations

Abstract

Metal inserts are widely used particularly in bolted connections for joining composite members. In this work, a theoretical basis is provided for analyzing the damping behavior of a cantilever composite square hollow member embedded with metal inserts along its length. Analytic stress solutions around the boundaries of the insert and the member are introduced while deriving the expression of modal damping ratio. Kelvin–Voigt and amplitude-dependent damping models are considered for the formulation. Experiments are performed on the perforated composite tube reinforced with brass, copper, and steel annular inserts subjected to transverse base motion of varying amplitudes. The acceleration responses recorded from the tests are analyzed to evaluate the damping ratio of the fundamental mode. It is observed that the damping ratio evaluated from the experiments matches well with the proposed value. Furthermore, it is found that the damping ratio increases when the holes are reinforced with the inserts. The reason for the increase in damping stems from (i) frictional effect at the boundaries of the insert and the tube and (ii) material damping of the inserts. For example, the damping amplification of the tube with five steel inserts is noted to be around 3.0 and 2.1 times with respect to the unperforated and perforated (with holes) cases, respectively.

Original languageEnglish
Pages (from-to)915-931
Number of pages17
JournalJVC/Journal of Vibration and Control
Volume28
Issue number7-8
DOIs
StatePublished - Apr 2022
Externally publishedYes

Funding

The authors would like to genuinely thank Prof. Bishakh Bhattacharya, Dept. of Mechanical Engineering, IIT Kanpur for emphasizing the importance of the problem. The authors would like to thank laboratory technicians and staff of the Structural Engineering Laboratory, Indian Institute of Technology Kanpur for their help and guidance during the work. The author(s) disclosed receipt of the following financial support for the research, authorship, and/or publication of this article: This work was partially supported by the Indian Space Research Organization (ISRO) through ISRO-IITK Space Technology Cell. The author(s) disclosed receipt of the following financial support for the research, authorship, and/or publication of this article: This work was partially supported by the Indian Space Research Organization (ISRO) through ISRO-IITK Space Technology Cell.

FundersFunder number
ISRO-IITK
Indian Space Research Organization
Indian Institute of Technology Kanpur
Indian Space Research Organisation

    Keywords

    • Composite tube
    • damping ratio
    • dynamic excitation
    • inserts

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