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# Deflection Coefficients

This section covers deflection coefficients, including deflection due to shear and the use of graphical methods.

## The Method Of Deflection Coefficients.

It can be seen that any beam of length $\inline&space;l$ and flexural rigidity $\inline&space;EI$ which carries a load $\inline&space;W$ (no mattter how it is distributed), will have a maximum deflection of $\inline&space;\displaystyle&space;\frac{W\,l^3}{E\,I}$ ; where $\inline&space;k$ is a constant which depends upon the type of loading and supports.

The value of $\inline&space;k$ has been found for the standard cases of a cantilever and a simply supported beam (See Deflection of Beams Part 1 Example 4 and Part 3 Example 1), and the deflection in other cases may frequently be built up by superposition.

Deflection is a term that is used to describe the degree to which a structural element is displaced under a load.

The Principle of Superposition: This states that where a number of loads act together on an elastic material, the resulting strain is the sum of the individual strains caused by each load acting separately.

Two types of problems will be solved by this method:

Example:
[imperial]
##### Example - Example 1
Problem
A beam of uniform section and length $\inline&space;2l$ is simply supported at its ends and by an elastic prop at the centre. If the prop deflects an amount $\inline&space;\displaystyle&space;\alpha$ times the load it carries and the beam carries a total uniformly distributed load $\inline&space;W$ show that the the load carried by the prop $\inline&space;\displaystyle&space;\frac{5\,W}{8\left(1&space;+&space;+\;6\,E\,I\,\alpha&space;/l^3&space;\right)}$

If $\inline&space;l&space;=&space;10\;ft.$ $\inline&space;I&space;=&space;15\;in^4$ $\inline&space;W&space;=&space;10,000\;lb.$ and $\inline&space;\alpha&space;&space;=&space;6.93\times10^{-4}\;in.lb.^{-1}$

Find the position and value of the maximum Bending Moment. $\inline&space;\displaystyle&space;E&space;=&space;30\times10^6\;lb.\,in^{-2}$

If $\inline&space;P$ is the load on the prop, then its deflection is $\inline&space;\displaystyle&space;\alpha&space;\;P$ carries a uniformly distributed load of 5 tons over its length of 10 ft. The beam is supported by three vertical steel tie rods each 6 ft. long, one at each end and one in the middle, the end rods having diameters of 1 in. and the centre rod 1.25 in.

Calculate the deflection at the centre of the beam below the end points and the stress in each tie rod. $\inline&space;\displaystyle&space;E&space;=&space;30\times&space;10^6&space;lb.&space;in^{-2}$

Workings
The downwards deflection due to the load only is : $\inline&space;\left(\displaystyle\frac{5}{384}&space;\right)\displaystyle\frac{W(2l)^3}{E\,I}$

The upwards deflection due to the prop only is: $\inline&space;\displaystyle\frac{P\,(2l)^3}{48\;E\,I}$

By superposition, the net downwards deflection is given by:
$\alpha&space;\;P&space;=&space;\left(\frac{5}{384}&space;\right)\frac{W(2l)^3}{E\,I}&space;-&space;\frac{P\,(2l)^3}{48\;E\,I}$
$\therefore\;\;\;\;\;\;P\left(\alpha&space;&space;+&space;\frac{l^3}{6\;E\.I}&space;\right)&space;=&space;\left(\frac{5}{48}&space;\right)\left(\frac{W\;l^3}{E\,I}&space;\right)$
Thus, $\inline&space;P&space;=&space;\displaystyle\frac{5\;W}{8(6\,E\,I\times&space;\displaystyle\frac{\alpha&space;}{l^3})}$

Substituting the numerical values given:

$P&space;=&space;\frac{5\times10,000}{8[(6\times30\times16^6\times15\times6.93\times10^{-4})/120^3&space;+&space;1]}$
$\therefore\;\;\;\;\;P&space;=&space;3000\;lb.$

The reaction at the end supportsis given by:

$R=\frac{1}{2}(10,000&space;-&space;3000)&space;=&space;3,500\;lb.$
And for $\inline&space;x&space;<&space;10&space;ft.$ ,$\inline&space;M=3500\;x&space;-&space;\left(\displaystyle\frac{10,000}{20}&space;\right)\left(\displaystyle\frac{x^2}{2}&space;\right)$

For a maximum $\inline&space;\displaystyle&space;\frac{dM}{dx}&space;=&space;0$

$\therefore\;\;\;\;\;\;x&space;=&space;\frac{3500}{500}&space;=&space;7\,ft.$
And $\inline&space;\hat{M}&space;=&space;12,250\;lb.ft.$
Solution
• The deflection is $\inline&space;P=3000\;lb.$
• The value of the maximum Bending Moment is $\inline&space;\hat{M}&space;=&space;12,250\;lb.ft.$

## Deflection Due To Shear

It can be shown that the shear stress set up in the transverse section of a beam and the accompanying shear strain will cause a distortion of the cross-section. Since the shear stress varies from zero at the extreme fibres to a maximum at the neutral axis, cross sections can no longer remain plane after bending.

A cantilever is a beam anchored at only one end. The beam carries the load to the support where it is resisted by moment and shear stress. Cantilever construction allows for overhanging structures without external bracing.

In fact the "warping" will be of the form shown in the diagram. The left-hand view being for positive shear and the right-hand for negative shear. These strains are incompatible with the theory of pure bending, but nevertheless a good approximation in deflection can be obtained by strain energy methods. It should also be noted that the shear distribution near to the application of a concentrated load must differ considerably from that given by the theory, since there can be no sudden change of shear strain from one type to the other, as would be implied for a simply supported beam with a central load.

Strain Energy due to Shear $\inline&space;\displaystyle&space;=&space;\frac{s^2}{2C}&space;\times&space;V$

And for the whole beam:
$U_s&space;=&space;\left(\frac{1}{2}C&space;\right)\int&space;\int&space;s^2\;Da.dx$

where $\inline&space;Da$ is an element of cross-section and $\inline&space;dx$ an element of the length.

The integration can only be performed for a particular cross-section over which the variation of $\inline&space;x$ is known and rectangular and $\inline&space;I$-sections will be calculated.

### Rectangular Section

It can be shown that using equation (1)
$U_s=\frac{1}{2C}\int&space;\left[\int_{-\frac{d}{2}}^{\frac{d}{2}}{\frac{36\,F^2}{b^2\,d^2}\left(\frac{d^4}{16}&space;-&space;\frac{d^2\;y^2}{2}&space;+&space;y^4&space;\right)b\;dy}&space;\right]\;dx$
$=\frac{1}{2C}\;\int\;\frac{36\;f^2}{b\;d^6}\left[\frac{d^4\;y}{16}&space;-&space;\frac{d^2\,y^3}{6}&space;+&space;\frac{y^5}{5}&space;\right]_{-\frac{d}{2}}&space;^{\frac{d}{2}}\;dx$
$=\frac{18}{C\,b\,d}\int&space;F^2\times&space;2\left(\frac{1}{32}&space;-&space;\frac{1}{48}&space;+&space;\frac{1}{160}&space;\right)\;dx=\frac{3}{5}\,C\,b\,d\int_{0}^{1}{F^2\;.dx}$

### For A Cantilever With A Load Of W At The Free End W = F

Thus from equation (2), $\inline&space;U_s&space;=&space;\displaystyle\frac{3\;W^2\;l}{5\;C\,b\,d}$

If
$\delta&space;_s$
is the deflection due to shear, then $\inline&space;U_s&space;=&space;\displaystyle\frac{1}{2}\;W\;\delta&space;_s$

### For A Cantilever With A Uniformly Distributed Load.

A load $\inline&space;\displaystyle&space;w\;\delta&space;x$ acting on a length $\inline&space;\displaystyle&space;\delta&space;x$ (situated at a distance $\inline&space;x$ from the fixed end) will produce a deflection due to shear at this point of $\inline&space;\displaystyle&space;\frac{\,w\,\delta&space;x.x}{5\;C\,b\,d}$ . For this load alone the distortion produced is indicated in the diagram, and is uniform for the shear force over the length $\inline&space;x$ and zero over the rest of the beam $\inline&space;(l&space;-&space;x)$. Hence the total deflection due to shear for all the distributed load is given by:
$\int_{0}^{1}{\frac{6\,w\,x\,dx}{5\;C\,b\,d}}&space;=&space;\frac{3\;w\,l^2}{5\;C\,b\,d}$

### For A Simply Supported Beam With Central Load W

A beam is a horizontal structural element that is capable of withstanding load primarily by resisting bending. The bending force induced into the material of the beam as a result of the external loads, own weight, span and external reactions to these loads is called a bending moment.

$F&space;=&space;\pm&space;\frac{W}{2}$

Thus by using equation (2) again, $\inline&space;U_s&space;=&space;\int_{0}^{1}{\displaystyle\frac{3(W^2/4)}{5\;C\,b\,d}.dx}$

$\;\frac{3W^2\;l}{20\;C\,b\,d}$
But since, $\inline&space;U_s&space;=&space;\displaystyle\frac{1}{2}\;W\;\delta&space;_s$

By substitution in equation (3 )

$\delta&space;_s&space;=&space;\frac{3\;W\;l}{10\;C\,b\,d}$

The simplified deflection is as shown in the upper diagram and since the shearing force is constant over each half, this case is equivalent to a cantilever of length $\inline&space;\displaystyle\frac{l}{2}$ carrying an end load of $\inline&space;\displaystyle\frac{W}{2}$.

If the load is not centrally applied but divides the length into $\inline&space;\displaystyle&space;l_1$ and $\inline&space;l_2$, then we can treat either end as a cantilever with an end load equal to the reaction on that side.

Hence, $\inline&space;\delta&space;_s&space;=&space;\displaystyle\frac{^\;(Wl_2/l_1)l_1}{5\;C\,b\,d}=&space;\displaystyle\frac{^\;W\;l_1\,l_2}{5\;C\,b\,d\,l}$

### A Simply Supported Beam With A Uniformly Distributed Load

Considering a load $\inline&space;w\;\delta&space;x$ only at a distance $\inline&space;x$ from one end $\inline&space;\displaystyle&space;\left(x\,<\,\frac{l}{2}\right)$ the deflection at the load will be:
$\frac{6\,w\,\delta&space;x\;(l&space;-&space;x)\,x}{5\;C\,b\,d\,l}$

Note this has already been proved in equation (4)
By proportion the deflection at the centre of the beam :
$\frac{6\,w\,\delta&space;x\;(l&space;-&space;x)\,x}{5\;C\,b\,d\,l}\left(\frac{l/2}{l&space;-&space;x}&space;\right)$

Then the total central deflection due to shear is:
$=&space;\int_{o}^{\frac{l}{2}}{\frac{3\,w\,x\,dx}{5\;C\,b\,d}}}&space;=&space;\frac{3\;w\;l^2}{20\;C\;b\,d}$

### I-section

The shear force is treated as being uniformly distributed over the web area.

Thus $\inline&space;\displaystyle&space;s&space;=&space;\frac{F}{b\,d}$ and $\inline&space;\displaystyle\int&space;dA&space;=&space;bd$ and using equation (1)

$\therefore\;\;\;\;\;\;U_s&space;=&space;\left(\frac{1}{2}C&space;\right)\int&space;\left(\frac{F^2}{b^2\;d^2}&space;\right)b\;d.dx=&space;\frac{(\int&space;F^2\;dx)}{2\;C\,b\,d}$

By similar methods to those used from a rectangular section the deflections due to shear may be obtained as follows:

• Cantilever with end load $\inline&space;\displaystyle&space;\delta&space;_s&space;=&space;\frac{W\;l}{C\;b\,d}$
• Cantilever with distributed load $\inline&space;\displaystyle&space;\delta&space;_s&space;=&space;\frac{W\;l}{2\;C\;b\,d}$
• Simply supported beam with central load $\inline&space;\displaystyle&space;\delta&space;_s&space;=&space;\frac{W\;l}{4\;C\;b\,d}$
• Simply supported beam with distributed load $\inline&space;\displaystyle&space;\delta&space;_s&space;=&space;\frac{W\;l}{8\;C\;b\,d}$

The Strain Energy method known as {Castigliano's Theorem} (See Bending of Curved Bars) may be used where a number of loads exist concurrently, or to find the distributed load by imposing a concentrated load at a deflection point; the latter giving it a value of zero. i.e.$\inline&space;\displaystyle&space;\delta&space;_s&space;=&space;\left(&space;\frac{\partial&space;U_s}{\partial&space;P}\&space;\right)_{p&space;=&space;0}$

Example:
[imperial]
##### Example - Example 1
Problem
For a given cantilever of rectangular cross-section, length $\inline&space;l$ and depth $\inline&space;d$ show that if $\inline&space;\displaystyle&space;\delta$ and $\inline&space;\delta&space;_s$ are the deflections due to shear and Bending due to a concentrated load at the free end, $\inline&space;\displaystyle&space;\frac{\delta&space;}{\delta&space;_s}&space;=&space;k\,.\,\left(\frac{d}{l}&space;\right)^2$ and find the value for $\inline&space;k$ for steel. $\inline&space;\displaystyle&space;E&space;=&space;30\times10^6\;lb.in^{-2}\;\;;\;\;C&space;=&space;11.5\times10^6\;lb.in.^{-2}$ .

Hence find the least value of $\inline&space;\displaystyle\frac{l}{d}$ if the deflection due to shear is not to exceed 1% of the total.
Workings
It has been shown that: $\inline&space;\delta&space;_s&space;=&space;\displaystyle\frac{6\;W\;l}{5\;C\;b\,d}$
$\delta&space;_b&space;=&space;\frac{W\;l^3}{3\;E\,I}&space;=&space;\frac{\;W\;l^3}{E\;b\;d^3}$

For a rectangular Section:
$\therefore\;\;\;\;\;\frac{\delta&space;_s}{\delta&space;_b}&space;=&space;\frac{6}{5\times4}\times\frac{E}{C}\times\left(\frac{d}{l}&space;\right)^2&space;=&space;k\left(\frac{d}{l}&space;\right)^2$
$\therefore\;\;\;\;\;k&space;=&space;\left(\frac{3}{10}&space;\right)\left(\frac{E}{c}&space;\right)&space;=&space;\left(\frac{3}{10}&space;\right)\left(\frac{30}{11.5}&space;\right)&space;=&space;0.783$

If $\inline&space;\displaystyle\frac{\delta&space;_s}{\delta&space;_p&space;+&space;\delta&space;_s}&space;=&space;0.01$

Then $\inline&space;\displaystyle\frac{\delta_s}{\delta&space;_P}&space;=&space;\displaystyle\frac{0.01}{0.99}&space;=&space;0.783\;\left(\displaystyle\frac{d}{l}&space;\right)^2$

The least value of $\inline&space;\displaystyle\frac{l}{d}&space;=&space;\sqrt{0.783\times99}&space;=&space;8.8$
Solution
• $\inline&space;k$ is $\inline&space;0.783$
• The least value of $\inline&space;\displaystyle\frac{l}{d}$ is $\inline&space;8.8$

## Deflection By Graphical Method

It was shown in the pages on "Shearing force and Bending Moment" that a Funicular Polygon could be used to perform a double integration of the load curve and this would produce the Bending Moment diagram.

Since $\inline&space;\displaystyle&space;\frac{d^2y}{dx^2}&space;=&space;\frac{M}{E\,I}$, it follows that a double integration of the Bending Moment curve will

produce the Deflection Curve.

If $\inline&space;EI$ is constant, draw the B.M. diagram and divide it into a number of strips of width$\inline&space;\displaystyle&space;\delta&space;x$. Now draw a vertical line to represent the areas $\inline&space;\displaystyle&space;M\delta&space;x$ and join this to a pole $\inline&space;O$ on the right of the line. Proceed in the normal way to draw the funicular polygon, which will be a series of straight lines to be smoothed out into a curve.The vertical ordinates on this diagram represent deflection and it will usually be necessary to slew the diagram through an angle in order to produce a horizontal base (e.g. from a simply supported beam)

If the scales are $\inline&space;\displaystyle&space;1\;in.&space;=&space;s_1\;lb.in^2\;\;\;M\;\delta&space;x\;units,\;1\,in.&space;=&space;s_2\;in.\;length$ and $\inline&space;1\;in.&space;=&space;s_3\;EIy\;units$, then the distance $\inline&space;h$ is given by $\inline&space;\displaystyle&space;\frac{s_3}{s_1\;s_2}\;in.$

If then the Deflection scale required is $\inline&space;\displaystyle&space;1\;in.&space;=&space;s_4\,in.&space;=&space;\frac{s_3}{EI}\;\;h&space;=&space;\frac{EI\;s_4}{s_1\;s_2}$