Introduction
In this lesson we will study a semi-graphical method refer to as the Moment-Area method developed by Charles E. Greene for finding deflection of beam using moment curvature relation.
\[{d \over {dx}}\left( {{{dy} \over {dx}}} \right)=-{M \over {EI}}\] (5.1)
\[\Rightarrow {\left( {{{dy} \over {dx}}} \right)_A}- {\left( {{{dy} \over {dx}}} \right)_B}=\int\limits_{{x_A}}^{{x_B}} {{{Mdx} \over {EI}}}\] (5.2)
where, \[{\left( {{{dy}/ {dx}}})_A}-{\left( {{{dy} / {dx}}} \right)_B}\] , hereafter referred to as \[{\theta _{AB}}\] is the angle between tangents at A and B as illustrated in Figure 5.1a. Similarly the deflection at B with respect to tangent at A, may be written as,
\[{\delta _{AB}}=\int\limits_{{x_A}}^{xB} {xd\theta }=\int\limits_{{x_A}}^{{x_B}} {{{Mxdx} \over {EI}}}\] (5.3)
It is to be noted that \[\int\limits_{{x_A}}^{{x_B}} {{{Mxdx}/{EI}}}\] represents the statical moment with respect to B of the total bending moment area between A and B, divided by EI. Therefore equation (5.3) may also be written as,
\[{\delta _{AB}}=\left[ {\int\limits_{{x_A}}^{{x_B}} {{{Mdx} \over {EI}}} } \right]\bar x\] , (5.4)
\[\Rightarrow {\delta _{AB}}=\bar x{\theta _{AB}}\] , (5.4)
where \[\bar x\] is the centroidal distance as shown in Figure 5.1a.
Fig. 5.1.
Based on equations (5.2) and (5.4) the moment-area theorem may be stated as,
Theorem 1
The change in slope between the tangents drawn to the elastic curve at any two points A and B is equal to the area of bending moment diagram between A and B, divided by EI.
Theorem 2
The deviation of any point B relative to the tangent drawn to the elastic curve at any other point A, in a direction perpendicular to the original position of the beam, is equal to the moment with respect to B of the area of bending moment diagram between A and B, divided by EI
Applications of the Moment-area theorem will now be demonstrated via several examples.
2 Example 1
A simply supported beam AB is subjected to a uniformly distributed load of intensity of q as shown in Figure 5.2. Calculate the deflection at the midspan. Flexural rigidity of the beam is EI.
Fig. 5.2.
Solution
From Example 4.1, bending moment at a distance x from A is,
\[{M_x}={{ql} \over 2}x - {{q{x^2}} \over 2}\] (4.4)
Due to symmetry slope of the elastic line at midspan is zero. Therefore
\[{\theta _{AC}} = {\theta _A} = \int\limits_{{x_A}}^{{x_C}} {{{{M_x}dx} \over {EI}}}={1 \over {EI}}\int\limits_0^{{{l/2}}} 2{\left( {{{ql} \over 2}x - {{q{x^2}} \over 2}} \right)dx}\]
\[\Rightarrow {\theta _A}={{q{l^3}} \over {24EI}}\]
Now since δ may be considered as the deflection at A with respect to tangent at C, we have,
\[\delta={\theta _A}\bar x = {{5q{l^3}} \over {384EI}}\]
3 Example 2
A cantilever beam AB is subjected to a concentrated load P at its tip as shown in Figure 5.3. Determine deflection and slope at B.
Fig. 5.3.
Solution
\[{\theta _{AB}}=\int\limits_{{x_A}}^{{x_B}} {{{{M_x}dx} \over {EI}}}={{P{l^2}} \over {2EI}}\]
Since slope at A is zero,
\[{\theta _B}={\theta _{AB}}=-{{P{l^2}} \over {2EI}}\]
\[\delta={\theta _B}\bar x={{P{l^2}} \over {2EI}}{{2l} \over 3}={{P{l^3}} \over {3EI}}\]
1. What is the moment-area method for calculating deflection of a beam? |
2. How is the moment-area method used in agricultural engineering? |
3. Can the moment-area method be used for all types of beams? |
4. How does the moment-area method account for variable loading along a beam? |
5. Are there any limitations or assumptions associated with the moment-area method? |
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