Journal ArticleDOI
Static and dynamic instability analysis of tapered CNTRC sandwich plates under uniform and non-uniform in-plane loadings using spline finite strip method
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TLDR
The buckling analysis of rectangular sandwich plates with pure polymeric tapered cores and functionally graded carbon nanotube (FG-CNT) reinforced composite face sheets under static and harmonic dynamic loads is presented in this article.About:
This article is published in Aerospace Science and Technology.The article was published on 2021-03-01. It has received 18 citations till now. The article focuses on the topics: Finite strip method & Dynamic load testing.read more
Citations
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Estimation of carbon nanotubes and their applications as reinforcing composite materials–An engineering review
TL;DR: In this article, a review has been carried regarding predicting material properties of single-walled carbon nanotubes (SWCNTs) using computational models and different approaches related to predicting the properties are discussed in detail.
Journal ArticleDOI
The effect of uncertainty sources on the dynamic instability of CNT-reinforced porous cylindrical shells integrated with piezoelectric layers under electro-mechanical loadings
TL;DR: In this paper, the influence of the propagation of different uncertainty sources on the dynamic stability of a sandwich carbon nanotube-reinforced (CNT) cylindrical shell under a pulse axial load is investigated.
Journal ArticleDOI
A semi-analytical nonlocal elasticity model for static stability and vibration behaviour of agglomerated CNTs reinforced nano cylindrical panel under non-uniform edge loads
C M Twinkle,Jeyaraj Pitchaimani +1 more
TL;DR: In this paper, a semi-analytical non-local elasticity model to analyze the effect of non-uniform edge loads on static stability and free vibration characteristics of agglomerated carbon nanotubes (CNTs) reinforced nano cylindrical panels is presented.
Journal ArticleDOI
A semi-analytical nonlocal elasticity model for static stability and vibration behaviour of agglomerated CNTs reinforced nano cylindrical panel under non-uniform edge loads
TL;DR: In this paper , a semi-analytical method to study agglomerated CNT composite cylindrical panels considering non-local elasticity is presented, and the results obtained using the present approach are in good agreement with the results available in literature.
Journal ArticleDOI
Thermo-mechanical postbuckling analysis of sandwich cylindrical panels with functionally graded auxetic GRMMC core supported by elastic foundations
Xiuhua Chen,Hui-Shen Shen +1 more
TL;DR: In this paper , the authors modeled and analyzed compressive and thermal postbuckling of sandwich cylindrical panels supported by an elastic foundation, where the compositional properties of both metal face sheets and the GRMMC core are assumed to be temperature dependent.
References
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Journal ArticleDOI
A Simple Higher-Order Theory for Laminated Composite Plates
TL;DR: In this paper, a higher-order shear deformation theory of laminated composite plates is developed, which accounts for parabolic distribution of the transverse shear strains through the thickness of the plate.
Journal ArticleDOI
Buckling analysis of functionally graded carbon nanotube-reinforced composite plates using the element-free kp-Ritz method
TL;DR: In this paper, the buckling analysis of functionally graded carbon nanotube-reinforced composite (FG-CNTRC) plates under various in-plane mechanical loads, using the element-free kp-Ritz method, is presented.
Journal ArticleDOI
Nonlinear vibration and bending of sandwich plates with nanotube-reinforced composite face sheets
Zhen-Xin Wang,Hui-Shen Shen +1 more
TL;DR: In this article, the authors studied the large amplitude vibration and the nonlinear bending of a sandwich plate with carbon nanotube-reinforced composite (CNTRC) face sheets resting on an elastic foundation in thermal environments.
Journal ArticleDOI
An efficient higher-order plate theory for laminated composites
Maenghyo Cho,R. Reid Parmerter +1 more
TL;DR: In this article, a higher-order plate theory for symmetric laminated composites is developed by superposing a cubic varying displacement field on a zig-zag linearly varying displacement.
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