Content uploaded by Mousa Khalifa
Author content
All content in this area was uploaded by Mousa Khalifa on May 07, 2019
Content may be subject to copyright.
This article was downloaded by: [King Khalid University]
On: 10 December 2014, At: 23:56
Publisher: Taylor & Francis
Informa Ltd Registered in England and Wales Registered Number: 1072954 Registered office: Mortimer House,
37-41 Mortimer Street, London W1T 3JH, UK
Mechanics of Advanced Materials and Structures
Publication details, including instructions for authors and subscription information:
http://www.tandfonline.com/loi/umcm20
Buckling Behavior under Radial Loading of Orthotropic
Oval Cylindrical Shells with Parabolically Varying
Thickness
Mousa Khalifa Ahmeda
a Department of Mathematics, Faculty of science at Qena, South Valley University, Egypt. E-
mail:
Accepted author version posted online: 18 Nov 2014.
To cite this article: Mousa Khalifa Ahmed (2014): Buckling Behavior under Radial Loading of Orthotropic Oval
Cylindrical Shells with Parabolically Varying Thickness, Mechanics of Advanced Materials and Structures, DOI:
10.1080/15376494.2014.949928
To link to this article: http://dx.doi.org/10.1080/15376494.2014.949928
Disclaimer: This is a version of an unedited manuscript that has been accepted for publication. As a service
to authors and researchers we are providing this version of the accepted manuscript (AM). Copyediting,
typesetting, and review of the resulting proof will be undertaken on this manuscript before final publication of
the Version of Record (VoR). During production and pre-press, errors may be discovered which could affect the
content, and all legal disclaimers that apply to the journal relate to this version also.
PLEASE SCROLL DOWN FOR ARTICLE
Taylor & Francis makes every effort to ensure the accuracy of all the information (the “Content”) contained
in the publications on our platform. However, Taylor & Francis, our agents, and our licensors make no
representations or warranties whatsoever as to the accuracy, completeness, or suitability for any purpose of the
Content. Any opinions and views expressed in this publication are the opinions and views of the authors, and
are not the views of or endorsed by Taylor & Francis. The accuracy of the Content should not be relied upon and
should be independently verified with primary sources of information. Taylor and Francis shall not be liable for
any losses, actions, claims, proceedings, demands, costs, expenses, damages, and other liabilities whatsoever
or howsoever caused arising directly or indirectly in connection with, in relation to or arising out of the use of
the Content.
This article may be used for research, teaching, and private study purposes. Any substantial or systematic
reproduction, redistribution, reselling, loan, sub-licensing, systematic supply, or distribution in any
form to anyone is expressly forbidden. Terms & Conditions of access and use can be found at http://
www.tandfonline.com/page/terms-and-conditions
ACCEPTED MANUSCRIPT
ACCEPTED MANUSCRIPT
1
Buckling Behavior under Radial Loading of Orthotropic Oval Cylindrical Shells with
Parabolically Varying Thickness
Mousa Khalifa Ahmed
Department of Mathematics, Faculty of science at Qena, South Valley University, Egypt.
E-mail: mossa@dr.com
ABSTRACT
In this paper, the framework of the Flügge’s shell theory, the transfer matrix approach and the
Romberg integration method has been employed to investigate the buckling analysis of radial
loaded oval cylindrical shell with parabolically varying thickness along of its circumference.
Trigonometric functions are used to form the modal displacements of the shell and Fourier’s
approach is used to separate the variables. The mathematical analysis is formulated to overcome the
difficulties related to mode coupling of variable curvature and thickness of the shell. Using the
transfer matrix of the shell, the buckling equations of the shell are reduced to eight first-order
differential equations in the circumferential coordinate and rewritten in a matrix form and solved
numerically. The proposed model is adopted to get the critical buckling loads and the corresponding
buckling deformations for the symmetrical and antisymmetrical modes of buckling. The influences
of the shell geometry, orthotropic parameters, ovality parameter, and thickness ratio on the buckling
parameters and the bending deformations are presented for different type-modes of buckling.
Downloaded by [King Khalid University] at 23:56 10 December 2014