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Building Design and Construction Handbook - Merritt - Ventech!

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5.70 SECTION FIVE<br />

As an example of the use of the method of least work, we shall solve again for<br />

the stress in the vertical bar in Fig. 5.50. Calling this stress X, we note that the<br />

stress in each of the inclined bars must be (P � X)/2 cos �. With the aid of Eq.<br />

(5.30), we can express the strain energy in the system in terms of X as<br />

2 2<br />

XL (P � X) L<br />

U � � 3<br />

2AE 4AE cos �<br />

Hence, the internal work in the system will be a minimum when<br />

�U XL (P � X)L<br />

� � � 0 3<br />

�X AE 2AE cos �<br />

Solving for X gives the stress in the vertical bar as P/(1 � 2 cos 3 �), as before<br />

(Art. 5.10.1).<br />

5.10.4 Dummy Unit-Load Method<br />

In Art. 5.2.7, the strain energy for pure bending was given as U � M 2 L/2EI in Eq.<br />

(5.33). To find the strain energy due to bending stress in a beam, we can apply this<br />

equation to a differential length dx of the beam <strong>and</strong> integrate over the entire span.<br />

Thus,<br />

L 2 M dx<br />

U � � (5.94)<br />

0 2EI<br />

If M represents the bending moment due to a generalized force P, the partial derivative<br />

of the strain energy with respect to P is the deformation d corresponding<br />

to P. Differentiating Eq. (5.94) under the integral sign gives<br />

L M �M<br />

d � � dx (5.95)<br />

0 EI �P<br />

The partial derivative in this equation is the rate of change of bending moment with<br />

the load P. It is equal to the bending moment m produced by a unit generalized<br />

load applied at the point where the deformation is to be measured <strong>and</strong> in the<br />

direction of the deformation. Hence, Eq. (5.95) can also be written<br />

L Mm<br />

d � � dx (5.96)<br />

0 EI<br />

To find the vertical deflection of a beam, we apply a vertical dummy unit load at<br />

the point where the deflection is to be measured <strong>and</strong> substitute the bending moments<br />

due to this load <strong>and</strong> the actual loading in Eq. (5.96). Similarly, to compute a rotation,<br />

we apply a dummy unit moment.<br />

Beam Deflections. As a simple example, let us apply the dummy unit-load<br />

method to the determination of the deflection at the center of a simply supported,<br />

uniformly loaded beam of constant moment of inertia (Fig. 5.51a). As indicated in<br />

Fig. 5.51b, the bending moment at a distance x from one end is (wL/2)x � (w/<br />

2)x 2 . If we apply a dummy unit load vertically at the center of the beam (Fig.

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