2018
DOI: 10.1177/1461348418756024
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Analytical model for flexural damping responses of CFRP cantilever beams in the low-frequency vibration

Abstract: In this paper, an analytical model for the flexural vibration damping of Carbon Fiber Reinforced Plastics (CFRP) cantilever beams was proposed, which is based on the Lamination Theory and Euler-Bernoulli Beam Theory. By using a finite element analysis and an analytical model, four sets of specific damping capacity with different pavement schemes were predicted, and flexural vibration test and damping analysis were carried out. Comparing the analytical model, finite element analysis, and test results, it could … Show more

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Cited by 9 publications
(8 citation statements)
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“…As for the CFRP laminated plate, only three damping loss factors are considered, the directions are shown in Figure 1. The damping loss factors in three direction of the laminated plate are as follows: η 11 = 0.82% η 22 = 2.98%, η 12 = 8.57% [21,22]. The damping loss factor of the structure is:…”
Section: Damping Ratiomentioning
confidence: 99%
See 1 more Smart Citation
“…As for the CFRP laminated plate, only three damping loss factors are considered, the directions are shown in Figure 1. The damping loss factors in three direction of the laminated plate are as follows: η 11 = 0.82% η 22 = 2.98%, η 12 = 8.57% [21,22]. The damping loss factor of the structure is:…”
Section: Damping Ratiomentioning
confidence: 99%
“…As for the CFRP laminated plate, onl are considered, the directions are shown in Figure 1. The d direction of the laminated plate are as follows: 𝜂 = 0.82% [21,22].…”
Section: Damping Ratiomentioning
confidence: 99%
“…η k ij (i, j � 1, 2, 3) shows the damping loss factors of anisotropic materials in six directions of the CFRP. e damping loss factor of the T700/YPH-42T material used in the CFRP motor frame is η 11 � 0.82%, η 22 � 2.98%, and η 12 � 8.57% [18]. Since the 2-3 plane of CFRP is isotropic, the damping loss factor in the shear direction of the material is considered to be equal; therefore, there is η 22 � η 33 and η 12 � η 13 � η 23 .…”
Section: Damping Of the Cfrp Motor Framementioning
confidence: 99%
“…Variety of FEM formulation theories such as firstorder shear deformation theory (FSDT), higher order shear deformation theory (HSDT), full layer wise displacement, 65 lamination theory, 68 and Euler-Bernoulli Beam Theory 68 are attempted by various researchers to investigate the vibration damping properties with different parameters. Biswas and Ray's 62 results of natural frequency show that first-order shear deformation theories had good correlation with ANSYS 14.0 and experimental for thin laminate and higher order shear deformation theories for thick laminates.…”
Section: Theoretical Modelingmentioning
confidence: 99%