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Steel Designers Manual - TheBestFriend.org

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This material is copyright - all rights reserved. Reproduced under licence from The <strong>Steel</strong> Construction Institute on 12/2/2007<br />

To buy a hardcopy version of this document call 01344 872775 or go to http://shop.steelbiz.<strong>org</strong>/<br />

<strong>Steel</strong> <strong>Designers</strong>' <strong>Manual</strong> - 6th Edition (2003)<br />

9.1.1 Equations of static equilibrium<br />

Element analysis 287<br />

From Newton’s law of motion, the conditions under which a body remains in static<br />

equilibrium can be expressed as follows:<br />

• The sum of the components of all forces acting on the body, resolved along any<br />

arbitrary direction, is equal to zero. This condition is completely satisfied if the<br />

components of all forces resolved along the x, y, z directions individually add up<br />

to zero. (This can be represented by SP x = 0, SP y = 0, SP z = 0, where P x, P y and<br />

Pz represent forces resolved in the x, y, z directions.) These three equations<br />

represent the condition of zero translation.<br />

• The sum of the moments of all forces resolved in any arbitrarily chosen plane<br />

about any point in that plane is zero. This condition is completely satisfied when<br />

all the moments resolved into xy, yz and zx planes all individually add up to zero.<br />

(SM xy = 0, SM yz = 0 and SM zx = 0.) These three equations provide for zero<br />

rotation about the three axes.<br />

If a structure is planar and is subjected to a system of coplanar forces, the<br />

conditions of equilibrium can be simplified to three equations as detailed below:<br />

• The components of all forces resolved along the x and y directions will individually<br />

add up to zero (SP x = 0 and SP y = 0).<br />

• The sum of the moments of all the forces about any arbitrarily chosen point in<br />

the plane is zero (i.e. SM = 0).<br />

9.1.2 The principle of superposition<br />

This principle is only applicable when the displacements are linear functions of<br />

applied loads. For structures subjected to multiple loading, the total effect of several<br />

loads can be computed as the sum of the individual effects calculated by applying<br />

the loads separately. This principle is a very useful tool in computing the combined<br />

effects of many load effects (e.g. moment, deflection, etc.). These can be calculated<br />

separately for each load and then summed.<br />

9.2 Element analysis<br />

Any complex structure can be looked upon as being built up of simpler units or<br />

components termed ‘members’ or ‘elements’. Broadly speaking, these can be<br />

classified into three categories:<br />

• Skeletal structures consisting of members whose one dimension (say, length) is<br />

much larger than the other two (viz. breadth and height). Such a line element is

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