BUCKLING OF RE-INFORCED ANISOTROPIC CYLINDRICAL SHELL WITH RINGS AND STRINGERS WITHOUT SHEAR LOAD
Author(s):
DR S BANIK, Dr Susmita Paul, Dr Sangita Das , Dr Jayanta chakraborty
Keywords:
Abstract
Solution of buckling of cylindrical shells in case of isotropic material is known from the literature on shells e.g. Flugge[1] (1973). An isotropic shell consists of composite materials such as Boron epoxy, re-inforced plastics and whiskers. They are used in many advanced structural applications and quite often in cylindrical shells. Buckling problem of an isotropic cylindrical shells has occupied the interest of many researchers such as Tasi[2] , Cheng & Kuenzi[3] , Hess T.E[4], Thielemann, Schnell and Fisher[5], Tasi, Fellmann and Strang[6], Cheng & Ho[7,8], Lie and Cheng[9], De,A[10-14]. The object of this paper is to formulate the differential equation for re-inforced anisotropic cylindrical shell of uniform thickness re-inforced by closely spaced rings or stringers or both. The corresponding solution of the differential equation so formulated is found out for shells without shear-load in the case of two-way compression.
Article Details
Unique Paper ID: 159508

Publication Volume & Issue: Volume 9, Issue 12

Page(s): 108 - 116
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