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# Comparative Study Of Results Obtained By Analysis Of Structures Using ANSYS, STAAD And MATLAB (Ref. CS0087) Introduction

The following discussion pertains to finite element analysis of 2 or 3 dimensional skeleton–like structures including trusses, frames, beams, etc. In general, trusses are structures whose elements can resist only axial forces. For practical purposes, all members in this discussion will be treated as beam elements capable of resisting bending moments, howsoever small these moments may be.

Frames are complex structures whose elements are beamelements capable of axial deformations as well. In this discussion, all elements are considered to be 2-noded 3 dimensional elements having 6 degrees of freedom at each node.In the local co-ordinate system, the element is oriented such that its lengthlies along the xaxis, while its cross-section lies in the yzplane. Thus at each node, the element is capable of axial deformation (local xaxis), transverse deformation (local yand zaxes) and rotation (about local x, yand zaxes). Since there are two nodes for each element, a 12×12 element stiffness matrix can be formed. This element stiffness matrix can be derived using the rod and beam element theory.

The Finite Element Method is an approximate method that uses computational tools to arrive at the solution of a problem. When the nature of the exact solution of an element is unknown, a simple function is chosen to represent it; this function is known as the interpolation model. The interpolation model is generally a polynomial, due to the ease with which it can be programmed and operated upon by calculus. However, such an interpolation model must satisfy certain convergence conditions in order that the approximate solution so produced,converges to the exact solutionon infinitely increasing the number of elements. The interpolation model of a uniaxial 2-noded rod element is thus linear, of the form:

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q= a0+ a1x(1.1)whereqis the axial displacementof a nodeat a distance xfroma reference origin, a0anda1are constants determined by boundary conditions of the element. The resulting stiffness matrix of the same element will thus be:

K = (EA/l) [1 -1-1 1](1.2)

where K denotes the element stiffness matrix, Eis the modulus of elasticity of the material of the element, A is the area of cross section of the element and lis the length of the element.

Since it is also a uniaxial phenomenon, the sameinterpolation model(equation 1.1)is used to determine torsional rotation with qrepresenting the angular displacement at a node. The corresponding stiffness matrix is:

Kt= (GJ/l) [1 -1-1 1] (1.3)

where Kt is the element stiffness matrix for torsion, Gis the shear modulus of the material of the element, J is the polar moment of inertia of the cross section of the material

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