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The composite damping capacity of sandwich cantilever beams

Investigation presents a forced-vibration method where by the displacement at free end of beam is measured by varying the frequency of the exciting motion at the fixed end. Damping properties of beam are determined by the resulting ratio of the two displacements

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Abstract

The governing equation of the flexural forced vibration of a cantilever sandwich beam excited by a sinusoidal displacement at the clamped end is developed by utilizing the conventional Hamilton's Principle. The effect of damping of the composite beam is incorporated into the elastic equation of motion by utilizing the Correspondence Principle of the linear viscoelastic theory. Several plots for different values of the composite damping factor are presented.

For comparison, an experimental setup was utilized to test different composite beams. The variation of the experimental results with those derived theoretically seem to be in agreement within the frequency range of the first few modes.

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Abbreviations

A :

area of core

A f :

area of face plates

G :

shear modulus of core

E :

elastic modulus of face plates

E * :

complex elastic modulus

E 1 :

storage modulus

E 2 :

loss modulus

L :

cantilever length of beam

I :

moment of inertia of face plates about the neutral axis of the beam

R a :

amplitude ratio

R f :

frequency ratio

U f :

strain energy of face plates

U o :

strain energy of core

U :

total strain energy

V :

kinetic energy of vibrating beam

Y o :

amplitude of forced exciting vibration

h :

thickness of face plates

c :

thickness of core

b :

width of beam

u :

extensional deformation of face plates

y :

vertical deflection

x :

coordinate in longitudinal direction

t :

time

m :

mass per unit length of beam

p :

real part of amplitude-ratio function

q :

imaginary part of amplitude-ratio function

γ:

shear strain

ω:

angular frequency

ω r :

resonant frequency

αL, βL :

complex Eigen mode functions

λ:

complex ratio of αL to βL

η:

specific energy loss per cycle

η1 :

composite damping coefficient

θ:

phase-lag angle

References

  1. Bert, C. W., Wilkins, D. J., and Crisman, W. C., “Damping in Sandwich Beams With Shear-Flexible Cores,” Proceedings of the Vibration Conference, American Society of Mechanical Engineers, Boston (March 1967).

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  5. Hoff, N. J., The Analysis of Structures, John Wiley and Sons, Inc. (1956).

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  7. Jones, I. W., Salerno, V. L., and Savacchio, A., “Evaluation of Damping Capacity of Sandwich Beams with Viscoelastic Cores,” Proceedings of the Annual ASME Meeting (November 1966).

  8. Kobayashi, S., “On Vibrations of Sandwich Beams,” Proceedings of the Fourth Japan National Congress of Applied Mechanics, Tokyo (1954).

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  11. Timoshenko, S., and Young, D. H., “Vibration Problems in Engineering,” D. Van Nostrand Co., Inc., Third Edition (1955).

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Shoua, E.D. The composite damping capacity of sandwich cantilever beams. Experimental Mechanics 8, 300–308 (1968). https://doi.org/10.1007/BF02326020

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  • DOI: https://doi.org/10.1007/BF02326020

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