2015
DOI: 10.1177/1099636215619841
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Free vibration analysis of fiber-reinforced polymer honeycomb sandwich beams with a refined sandwich beam theory

Abstract: Free vibration of a fiber-reinforced polymer honeycomb sandwich beam with sinusoidal core configuration is studied based on a refined sandwich beam theory. Using a micro/macromechanics approach for face laminates and a mechanics of material approach for honeycomb core, the equivalent elastic properties of face laminates and honeycomb core are obtained. A free vibration model based on the refined sandwich beam theory is formulated using the Hamilton's variational principle. Analytical solutions for a cantilever… Show more

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Cited by 27 publications
(17 citation statements)
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“…Shi Cheng et al [13] Based on a refined sandwich beam theory studied Free vibration of a fibrereinforced polymer honeycomb sandwich beam with sinusoidal Core configuration. Using a micro/macromechanics approach for face laminates and a mechanics of material approach for honeycomb core, the equivalent elastic properties of face laminates and honeycomb core are obtained.…”
Section: Beamsmentioning
confidence: 99%
“…Shi Cheng et al [13] Based on a refined sandwich beam theory studied Free vibration of a fibrereinforced polymer honeycomb sandwich beam with sinusoidal Core configuration. Using a micro/macromechanics approach for face laminates and a mechanics of material approach for honeycomb core, the equivalent elastic properties of face laminates and honeycomb core are obtained.…”
Section: Beamsmentioning
confidence: 99%
“…The simply supported boundary conditions for the uniformly distributed load can be written as: (29) By applying the boundary conditions above, one can fully determine the 10 unknown constants. The exact solution of the bending and the shear deflection can be written as: (30) The coefficients and are shown in the Appendix (A2).…”
Section: Uniformly Distributed Load Over the Platementioning
confidence: 99%
“…Compared with the FSDT, the RPT leads to a parabolic shear deformation distribution across the thickness direction thus automatically satisfy the traction free conditions. Therefore, it not only reduces the number of unknowns but also shows a clearer physical meaning and provides more accurate solutions than FSDT [30].…”
Section: Introductionmentioning
confidence: 99%
“…In addition, their mechanical behavior can be optimized by ingeniously choosing the material type and composite pattern. A typical application is the sandwich structures [1][2][3][4][5], usually composed of two stiff face layers and a relatively soft core layer, bonded together by the adhesive. It is known that the interfacial damage exists widely in sandwich structures due to the discontinuity of material property at the interface.…”
Section: Introductionmentioning
confidence: 99%