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D. Shaw

Other affiliations: Georgia Institute of Technology
Bio: D. Shaw is an academic researcher from National Tsing Hua University. The author has contributed to research in topics: Orthotropic material & Isotropy. The author has an hindex of 8, co-authored 10 publications receiving 212 citations. Previous affiliations of D. Shaw include Georgia Institute of Technology.

Papers
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Journal ArticleDOI
TL;DR: In this paper, the nonlinear analysis of geometrically imperfect, thin, laminated, circular, cylindrical shells subjected to uniform axial compression, and for various in-plane and transverse supports, is presented.

58 citations

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TL;DR: In this paper, the free vibration of rotating rectangular plates, with the effects of hub size, rotating speed, and setting angle accounted for, is studied, where the plate is considered to be clamped at the rim of a central hub and is free along the other three edges.

34 citations

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TL;DR: In this article, the accuracy of Donnell's equations for the buckling analysis of imperfect (limit point instability), circular, cylindrical, thin orthotropic shells under axial compression is investigated by comparing critical loads obtained by employing Donnell-type kinematic equations with those based on the more accurate Sanders-type.

29 citations

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TL;DR: In this article, the free vibration of rotating rectangular plates with an exponentially varying thickness is studied, where the plate is clamped at the rim of a central hub and is free along the other three edges.

27 citations

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TL;DR: In this paper, the imperfection sensitivity of thin cylindrical shells, made out of fiber-reinforced composite material and subjected to uniform axial compression, and the effects upon it of certain parameters, are investigated.

19 citations


Cited by
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Journal ArticleDOI
TL;DR: A review of recent research advances and trends in the area of thin shell buckling can be found in this paper, where the authors provide a personal view point on the buckling behavior of shells.
Abstract: This paper provides a review of recent research advances and trends in the area of thin shell buckling. Only the more important and interesting aspects of recent research, judged from a personal view point, are discussed. In particular, the following topics are given emphasis: (a) imperfections in real structures and their influence; (b) buckling of shells under local/non-uniform loads and localized compressive stresses; and (c) the use of computer buckling analysis in the stability design of complex thin shell structures. I INTRODUCTION Thin-shell structures find wide applications in many branches of engineering. Examples include aircraft, spacecraft, cooling towers, nuclear reactors, steel silos and tanks for bulk solid and liquid storage, pressure vessels, pipelines and offshore platforms. Because of the thinness of these structures, buckling is often the controlling failure mode. It is therefore essential that their buckling behavior be properly understood so that suitable design methods can be established. This paper provides a review of recent research advances and trends in the area of thin shell buckling. The paper is not intended to be an exhaustive review of the field, nor is it possible to do so in a single paper of limited length. Instead, only the more important and interesting aspects of recent research, judged from a personal viewpoint, will be discussed. In particular, the following topics are given emphasis: (a) imperfections in real structures and their influence; (b) buckling of shells under local/non-uniform loads and localized compressive stresses; and (c) the use of computer buckling analysis in the stability design of complex thin shell structures. The author wishes to apologize in advance for any inadvertent omission of relevant publications.

200 citations

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TL;DR: In this paper, a survey of the general area of buckling and postbuckling of thin-walled, geometrically imperfect, cylinders of various constructions, when subjected to destabilizing loads is presented.
Abstract: Thin-walled cylinders of various constructions are widely used in simple or complex structural configurations. The round cylinder is commonly found in tubing and piping, and in offshore platforms. Depending on their use, these cylinders are subjected (in service) to individual and combined application of external loads. In resisting these loads the system is subject to buckling, a failure mode which is closely associated with the establishment of its load-carrying capacity. Therefore, the system buckling and postbuckling behavior have been the subject of many researchers and investigators both analytical and experimental. The paper is a state-of-the-art survey of the general area of buckling and postbuckling of thin-walled, geometrically imperfect, cylinders of various constructions, when subjected to destabilizing loads. The survey includes discussion of imperfection sensitivity and of the effect of various defects on the critical conditions.

158 citations

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TL;DR: In this article, the exact closed form characteristic equations are given within the validity of the Mindlin plate theory for plates having two opposite sides simply supported, and the effect of boundary conditions, aspect ratios and thickness ratios on the eigenfrequency parameters and vibratory behavior of each distinct cases are studied in detail.

138 citations

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TL;DR: In this article, a postbuckling analysis for a functionally graded composite cylindrical shell reinforced by single-walled carbon nanotubes (SWCNTs) subjected to torsion in thermal environments is presented.

96 citations

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TL;DR: In this paper, a boundary layer theory for the buckling and postbuckling of anisotropic laminated thin shells is developed, which includes the effects of nonlinear prebuckling deformations, large deflections in the post-buckling range, and initial geometric imperfections of the shell.

95 citations