Composite Structures 3 1985
DOI: 10.1007/978-94-009-4952-2_50
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Large Amplitude Forced Vibration Response of Laminated Composite Rectangular Plates by a Finite Element Method

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Cited by 5 publications
(4 citation statements)
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“…Gary et al [13] studied large-amplitude vibrations and random responses of symmetrically laminated rectangular plates. Wentz et al [35] studied large-amplitude forced vibrations of laminated composite rectangular plates by a finite-element method. Eslami and Kandil [12] used the method of multiple scales to study the nonlinear response of an orthotropic panel to a harmonic excitation.…”
Section: Introductionmentioning
confidence: 99%
“…Gary et al [13] studied large-amplitude vibrations and random responses of symmetrically laminated rectangular plates. Wentz et al [35] studied large-amplitude forced vibrations of laminated composite rectangular plates by a finite-element method. Eslami and Kandil [12] used the method of multiple scales to study the nonlinear response of an orthotropic panel to a harmonic excitation.…”
Section: Introductionmentioning
confidence: 99%
“…al 1985 Present a finite element formulation for examining the large amplitude, steady-state, forced vibration response of arbitrarily laminated composite rectangular thin plates. [1] To analysis nonlinear forced vibration laminated composite rectangular plate, the nonlinear stiffness and harmonic force matrices has been developed and parametric variation in form of laminate angles and number of plies, in-plane boundary conditions has also been presented. The FE results are compared with available approximate continuum solutions.…”
Section: Literature Surveymentioning
confidence: 99%
“…(25) into Eq. (21) and equating coefficients of like powers of e yields The general solution to Eq. (54) can be expressed as…”
Section: Case Of 12 Near Onmentioning
confidence: 99%
“…This method also is used to solve the nonlinear forced vibration of symmetrically laminated rectangular plates by Mei and Chiang. 20 Later, Wentz et al 21 presented the forced vibration response of a generally laminated rectangular plate.…”
Section: Introductionmentioning
confidence: 99%