Recent Advances in Analysis of Laminated Beams and Plates, Part II: Vibrations and Wave Propagation

Kapania, Rakesh K.; Raciti, Stefano

doi:10.2514/3.59909

Cited by 264 publications

(83 citation statements)

References 160 publications

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“…A review was conducted on advances in analysis of laminated beams and plates vibration and wave propagation (Kapania and Raciti, 1989. Another review was done on the published literature of vibrations of curved bars, beams, rings and arches of arbitrary shape which lie in a plane (Chidamparam and Leissa, 1993).…”

Section: Dynamic Analysismentioning

confidence: 99%

Mechanics of Composite Beams

Hajianmaleki¹,

Qatu²

2011

Advances in Composite Materials - Analysis of Natural and Man-Made Materials

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Section: Dynamic Analysismentioning

confidence: 99%

Mechanics of Composite Beams

Hajianmaleki¹,

Qatu²

2011

Advances in Composite Materials - Analysis of Natural and Man-Made Materials

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“…An advanced model was proposed in [31] where classical finite beam elements were improved by introducing new degrees of freedom to describe the crosssection behavior. Other refined beam models can be found in the excellent reviews by Kapania and Raciti [32][33], which focused on: bending, vibration, wave propagations, buckling and post-buckling. Excellent papers on structural dynamic and aeroelastic problems of thin-walled structures by means of higher-order beams are those by Librescu [34][35][36].…”

Section: Introductionmentioning

confidence: 99%

Advanced 1D Structural Models for Flutter Analysis of Lifting Surfaces

Petrolo¹

2012

International Journal of Aeronautical and Space Sciences

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An advanced aeroelastic formulation for flutter analyses is presented in this paper. Refined 1D structural models were coupled with the doublet lattice method, and the g-method was used for flutter analyses. Structural models were developed in the framework of the Carrera Unified Formulation (CUF). Higher-order 1D structural models were obtained by using Taylor-like expansions of the cross-section displacement field of the structure. The order (N) of the expansion was considered as a free parameter since it can be arbitrarily chosen as an input of the analysis. Convergence studies on the order of the structural model can be straightforwardly conducted in order to establish the proper 1D structural model for a given problem. Flutter analyses were conducted on several wing configurations and the results were compared to those from literature. Results show the enhanced capabilities of CUF 1D in dealing with the flutter analysis of typical wing structures with high accuracy and low computational costs.

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“…A detailed review of several theories for vibrations and wave propagation was presented by Kapania and Raciti [20]. A first formulation of a second-order theory by using crosssectional warping and transverse direct stress was proposed by Stephen and Levinson [28].…”

Section: Introductionmentioning

confidence: 99%

Static and Dynamic Analysis of a Thin-Walled Layered Cylinder by Refined 1d Theories

Varello¹,

Carrera²

2014

Proceedings of 10th World Congress on Computational Mechanics

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Abstract. This paper presents an application of refined one-dimensional (1D) models to the static and free vibration analysis of thin-walled layered structures. Carrera Unified Formulation (CUF) is employed to easily introduce higher-order 1D models with a variable order of expansion for the displacement unknowns over the beam cross-section. Classical Euler-Bernoulli beam theory is obtained as a particular case of these variable kinematic models while a higher-order expansion permits the detection of the in-plane cross-section deformation. Finite element (FE) method is used to provide numerical results. In particular, the case of a deformable clamped-clamped thin-walled layered cylinder loaded by a non-uniform internal pressure is discussed. The static analysis reveals the model capabilities in accurately describing the three-dimensional deformation of the cylinder. The free vibration analysis provides results not detectable by typical 1D models in excellent agreement with a solid (3D) FE solution. The present models do not introduce additional numerical problems with respect to classical beam theories. Moreover, the results clearly show that finite elements which are formulated in the CUF framework offer shell-type capabilities in analyzing thin-walled structures with a remarkable reduction in the computational cost required.

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Recent Advances in Analysis of Laminated Beams and Plates, Part II: Vibrations and Wave Propagation

Cited by 264 publications

References 160 publications

Mechanics of Composite Beams

Mechanics of Composite Beams

Advanced 1D Structural Models for Flutter Analysis of Lifting Surfaces

Static and Dynamic Analysis of a Thin-Walled Layered Cylinder by Refined 1d Theories

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