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Deflections - Method of Virtual Work
Vertical Deflection of a Beam - Cantilever


The following example utilizes the cantilever method to determine the "real" and virtual moment diagrams used in the calculation of deflections of a beam.

Note: The colors of the loads and moments are used to help indicate the contribution of each force to the deflection or rotation being calculated. The moment diagrams show the moments induced by a load using the same color as the load.


problem statement

Determine the vertical displacement at end C of the beam shown in the figure below. The modulus of elasticity (E) and the moment of inertia (I) are constant for the entire beam.

A diagram showing a beam loaded with a concentrated force and applied moment
Figure 1 - Beam structure to analyze


Solution:

Calculate the support reactions (caused by the applied "real" loads) using the following relationships.

Equations

Check these reactions by summing the forces in the vertical direction.

shear equation

The resulting system,

Loaded beam with reactions
Figure 2 - Beam structure with reactions


The resultant shear and moment diagrams can be determined using statics (see figures below).

Resultant shear and moment diagram
Figure 3 - Resultant shear and moment diagrams

In this example we will use the cantilever method find an equivalent moment diagram in order to carry out the required integration.

To construct the moment diagrams caused by the applied "real" loads utilizing the cantilever method, a point on the structure is selected and a fixed support is assumed at this location.  In this example, point B is selected and a fixed support is inserted (see figure below).

Notice that all reaction forces are applied as loads on the structure with the assumed fixed support at B.

a diagram showing the fixed beam
Figure 4 - Cantilever beam structure

Plot the moment diagram for each applied load separately, i.e., by parts. The final results can then be obtained by utilizing the method of superposition i.e., by summing the contribution of each individual load to the displacement being calculated. This method is applicable since the structure is assumed to be elastic and the deflections are small.

Note: The centroid of each area is indicated by the numbered arrow and dot.

i) Moment diagram due to the 56 ft-k concentrated moment at A,

moment diagram for the 56 ft-k moment
Figure 5 - Moment diagram due to 56 ft-k moment

ii) Moment diagram due to the 2 k/ft applied load,

For the 2 k/ft applied load
Figure 6 - Moment diagram due to 2 k/ft applied load

iii) Moment diagram due to the 21 k support reaction at A,

For the 21 k support reaction
Figure 7 - Moment diagram due to 21k support reaction

iv) Moment diagram due to the 6k applied load at end C

For the 6 k applied load
Figure 8 - Moment diagram due to 6k applied load

Notice that the resultant moment diagram (figure 3 above) is the sum of these four diagrams.

resultant moment
Figure 9 - Resultant moment diagram


Apply the virtual load at the point of interest in the desired direction. In this case, apply a unit load at point C in the vertical direction. (see figure below)

Beam with an applied unit force at point D
Figure 10 - Beam with virtual load applied


Following the same procedure as used previously, calculate the support reactions (caused by the virtual load).

Sum the moments about A and B.

Equations

Check these reactions by summing the vertical forces.

shear equations

The resulting system,

Beam diagram with reactions
Figure 11 - Support reactions due to unit load


Determine the moment diagram due to the virtual load using the same procedure used to draw the "real" moment diagram i.e., with a fixed support assumed at point B.

Beam diagram with reactions
Figure 12 - Virtual unit load on cantilever structure

The resulting moment diagram due to the virtual load.  

 
Figure 13 - Moment diagram on cantilever structure due to virtual unit load


Once the "real" moment diagrams are determined, calculate the area enclosed by each moment diagram and determine the location of the centroid of each of these areas.

Area No. Area/EI (k-ft2/EI) Location of centroid
from support B (ft)
1. -56x20/EI=-1120/EI X1 = 1/2x20 = 10
2. 1/3x20x-400/EI=-2666.67/EI X2 = 1/4x20 = 5
3. 1/2x20x420/EI=4200/EI X3 = 1/3x20 = 6.67
4. 1/2x6x-36/EI=-108/EI X4 = 1/3x6   = 2

Determine the values - heights (hi) - on the virtual moment diagram (m) at the centroids of the moments due to the real loads. This is needed to carry out the integration by using the equation given in the introduction,

 virtual work equation

Proportions can be used to determine these heights (hi) on the moment diagram (m). For example, using similar triangles from the shared angle (location of  X1, X2, X3 & X4 were determined previously)

Proportions


Figure 14 - Heights on virtual load diagram

The heights (hi) are shown in the figure above at the locations of the centroids of the corresponding areas from the moment diagrams (M).


Integrate the equation , by using the visual integration approach.

Multiply the areas of the "real" moment diagram by the heights of the virtual moment diagram and add them together.

Area No. Area (a)
from M diagram (k-ft2/EI)
Height (h)
from m diagram (k-ft)
Ai*hi (k2-ft3/EI)
1. -1120/EI -3 3360/EI
2. -2666.67/EI -4.5 12000/EI
3. 4200/EI -4 -16800/EI
4. -108/EI -4 432/EI
Total -1008/EI

Since EI is constant throughout the structure, the total deflection at C equals -1008 k2-ft3/EI.

The negative sign indicates that the displacement is opposite to the direction of the unit load that was applied at C - therefore the deflection is upward.

If values of E and I are specified, the vertical deflection at C in inches can be determined.  For example, let E = 29,000 ksi, I = 144 in4, and Q = 1 k, then

equation


Contact Dr. Fouad Fanous for more information.