Abstract
Constrained layer damping is one of the passive techniques to control amplitude of vibration of structural components. In the present work an attempt has been made to quantify and compare damping ratios of composite-rubber-composite sandwich beam with that of pristine composite beam having nearly the same flexural stiffness and range of frequency of vibration from 20 Hz to 100 Hz. Length and thickness of sandwich and pristine beams in order to have the same flexural stiffness and desired frequency range of vibration were specifically designed. The damping ratio of each sandwich and pristine composite beams were measured experimentally using logarithmic decay and half-power bandwidth techniques.
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Abbreviations
- t c :
-
thickness of composite
- t b :
-
thickness of rubber
- t :
-
total thickness of the beam
- b :
-
width of the beam
- w t :
-
total vertical deflection
- w b :
-
vertical deflection due to bending
- w s :
-
vertical deflection due to shear deformation
- P :
-
point load
- E :
-
Young’s modulus
- E r :
-
Young’s modulus of rubber
- E c :
-
Young’s modulus of composite
- G :
-
Shear modulus
- υ :
-
Poisson’s ratio
- L :
-
length of the beam
- A :
-
cross-sectional area of the beam
- α s :
-
shear correction factor
- I :
-
area moment of inertia
- G eq :
-
equivalent shear modulus
- G r :
-
shear modulus of rubber
- G c :
-
shear modulus of composite
- z :
-
distance measured from neutral axis
- k CRC :
-
flexural stiffness of sandwich beam
- ω :
-
circular frequency
- f :
-
frequency
- ρ :
-
density
- A n :
-
amplitude at time n
- A n+1 :
-
amplitude at time n+1
- ξ :
-
damping ratio
- Q :
-
quality factor
- f 1 :
-
lower frequency
- f 2 :
-
upper frequency
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Chennamsetti, R., Hood, A., Guruprasad, S. et al. Damping ratios of pristine composite beam and constrained layer damped composite beam of equal stiffness. Int. J. Precis. Eng. Manuf. 14, 1655–1660 (2013). https://doi.org/10.1007/s12541-013-0224-6
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DOI: https://doi.org/10.1007/s12541-013-0224-6