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COMPOUND STRESSES AND STRAINS

Compound Stresses and Strains

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Page 1: Compound Stresses and Strains

COMPOUND STRESSES AND STRAINS

Page 2: Compound Stresses and Strains

CONTENTS

Introduction Principal Planes Principal Stresses Methods for the stresses on an oblique section

of a body Analytical method: Sign conventions for analytical method Stresses on an oblique section of a body Graphical method: Sign conventions for graphical method Mohr’s circle for stresses on an oblique section

of a body

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INTRODUCTION

We have already studied in detail the direct tensile and compressive stress as well as simple shear. In this we consider the stress in a plane which is at right angles to the line of action of force(tensile or compressive). But the majority of engineering, component and structures are subjected to such loading conditions or sometimes are of such shapes that there exists a complex state of stresses involving direct tensile, compressive as well as shear stresses in various directions. Here we study the nature and intensity of stresses on planes at angles other than right angles to the line of action of force.

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PRINCIPAL PLANES

At any point in a strained material, there are three planes, mutually perpendicular to each other, which carry direct stresses only and no shear stress.

These particular planes which have no shear stress are known as principal planes.

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PRINCIPAL STRESS

The magnitude of direct stress across the principal plane is known as principal stress

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METHODS FOR THE STRESSES ON AN OBLIQUE SECTION OF A BODY

The two methods are: Analytical method Graphical method

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ANALYTICAL METHOD

A body subjected to uniaxial direct stress A body subjected to biaxial direct stress A body subjected to general two dimensional

stress system

Sign conventions: All the tensile stresses and strains are taken

as positive whereas all the compressive stresses and strains are taken as negative.

The shear stress which tends to rotate the element in the clockwise direction is taken as positive and anticlockwise as negative

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STRESSES ON AN OBLIQUE SECTION OF A BODY SUBJECTED TO A DIRECT STRESS IN ONE PLANE (UNIAXIAL)

Consider a rectangular body of uniform cross section and unit thickness subjected to a direct tensile stress along x-x axis. Now let us consider an oblique section AB inclined with the x-x axis

Let =tensile stress across the face AC θ=angle which oblique section AB makes with BC ie with the x-x axil in the clockwise direction

A

BC

Page 9: Compound Stresses and Strains

Consider the equilibrium of the wedge ABC as shown in the figure

Horizontal force acting on the face AC

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BIBLIOGRAPHY