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2-8 Deformation of a Beam—Continuously Deformable Model







If you differentiate a quadratic function such as



y = ax2 + bx + c (2.8.1)



you will obtain



dy/dx = 2ax + b (2.8.2)



As shown in Fig. 2-8-1a, dy/dx represents the slope of the curve defined by the function. If you



differentiate it again, you will obtain



d2y/dx2 = 2a (2.8.3)



As shown in Fig. 2-8-1b, the radius of the curve corresponding to Eq. 2.8.3 is reduced as the



constant a increases. If a is negative, the curve is bent in the opposite direction. If the curve is



defined by trigonometric ( y  sin x ) or exponential ( y  e x ) functions, the term d2y/dx2 also



indicates how the curve is bent.

y

dy/dx

dy



x

0 dx

(a) Slope of a curve

y

Large a



Small a

0 Negative a x

(b) Various curves

Fig. 2-8-1 Quadratic functions Fig. 2-8-2 Cantilever beam







182

The broken line in Fig. 2-8-2a shows the deflected shape of the beam axis. The deflection at a



distance x from the fixed end is denoted as v. Figure 2-8-2b shows the deflection v as a function of



x, the distance from the fixed end. The first-order differential of the deflection,



dv

 (2.8.4)

dx



represents the slope of the beam axis. As we did in Section 2-6, we shall again assume that the



planes P1 and P2 in Fig. 2-8-2a remains perpendicular to the beam axis, and define the unit



curvature as



d

 (2.8.5)

dx



Note that Eq. 2.8.5 is equivalent to Eq. 2.6.1 (    / a ) except that the curvature is defined in an



infinitesimal region dx rather than a finite region a. Substituting Eq. 2.8.4 into Eq. 2.8.5 leads to:



d 2v

 2 (2.8.6)

dx



In other words, the second-order differential of the deflection indicates how the beam bends1 or









1

Equations 2.8.5 and 2.8.6 are approximate. The exact definition of unit curvature is

d

 (2.8.7)

ds

where ds is the length of the curve shown in Fig. 2-8-3. Therefore, the curve with a constant

curvature is a circle. Using some techniques of calculus, we get:

3/ 2

d 2v   dv 2 

 2 1     (2.8.8)

dx   dx  

 

In the case of beam deflection, however, dv/dx is very small so that squaring it makes it negligible;

and thus we can assume  = d2v/dx2.

183

how the slope changes over a very small distance ( d / dx ).







Recalling Eq. 2.6.4 ( M  EI ), we have:



d 2v M

 (2.8.9)

dx 2 EI



This result should be compared with Eq. 2.7.1, where the deformation of the beam is evaluated





within a finite region a. Equation 2.8.9 deals with the bending deformation within an infinitesimal



region dx. Solving this differential equation, we can determine the deflection of the beam. This is



equivalent to assuming an infinite number of springs representing the deformation within an



infinitesimal region dx.









Example 2-8-1: Assume that a cantilever beam is subjected to a couple M at its free end (x = l).



Determine the maximum slope and the maximum deflection of the beam.









Fig. 2-8-4 A couple at the free end









Fig. 2-8-3 Exact definition of curvature

184

Solution: First, we attempt to visualize how the beam would bend. The bending moment is



distributed uniformly as shown in Fig. 2-8-5a. The section does not change. We conclude that the



curvature is uniform along the beam. Inspecting the sense of the applied moment, we conclude that



the top fiber will be in compression and that the beam will bend into a shape concave upward.



From this information, we infer that the beam will bend as sketched in broken lines and that the



maximum slope and deflection will be at the free end.









We obtain the unit-curvature distribution using the expression d2v/dx2 = M/EI (Fig. 2-8-5b).



Integrating this expression yields the slope



dv M

  x  C1

dx EI



where C1 is a constant of integration. Because the slope is zero at the fixed end (dv/dx = 0 at x = 0),



we have C1 = 0. The slope  = dv/dx is distributed linearly along the span (Fig. 2-8-5c). Integrating



the expression for the slope and noting that the deflection is zero at the fixed end (v = 0 at x = 0),



we get the following result.



M

v  x2

EI



The slope and the deflection at the free end (x = L) are



ML

 (2.8.9) and

EI

ML2

v (2.8.10)

EI









185

Fig. 2-8-5







Exercise: Using the last two digits of your ID ij to change the couple to C  (i  2)  100



N-mm and the depth to h = (j + 5) mm, solve the example above again.









Example 2-8-2: Assume that a cantilever beam is subjected to a force F at the free end ( x = L).



Determine the slope and the deflection of the beam at the free end.









Fig. 2-8-6 A force at the free end









Solution: The bending moment varies linearly along the span as shown in Fig. 2-8-7a:



M  F   L  x



186

Use of  = M/EI leads to the unit-curvature distribution shown in Fig. 2-8-7b:



d 2v F

  L  x

dx 2 EI









Fig. 2-8-7



Integrating this equation and noting that the slope is zero at the fixed end (dv/dx = 0 at x = 0), we



have



dv F  x2 

  Lx   (2.8.11)

dx EI  2



The slope at the free end (x = L) is given by the following equation.



FL2

 (2.8.12)

2 EI



Integrating Eq. 2.8.12 and noting that the deflection is zero at the fixed end (v = 0 at x = 0), we



have



F  Lx 2 x3 

v    (2.8.13)

EI  2 6



The deflection at the free end (x = L) is given by the following equation.





187

FL3

v (2.8.14)

3EI



If you substitute the default values used in GOYA-C (F = 10 N, L = 100 mm, b = 10 mm, h = 15



mm, and E =100 N/mm2), you should get v = 11.9 mm. Check it using GOYA-C.









Exercise: Use the last two digits of your ID ij to change the force to F  (i  2) N and the



depth to h = (j + 5) mm. Calculate the slope and deflection at mid-span and at the free end.





Example 2-8-3: A force F is applied at mid-span of a cantilever beam. Calculate the slope and



deflection at the free end.









Fig. 2-8-8 A load at mid-span







Solution: The bending moment varies linearly between 0 200 > 500 > 1,000 > 2,000

5,000 > 10,000 > 20,000 > 200,000

Major All Star MVP Hall of Fame



Fig. 2-8-14









Design your own beam (Part 5): We want to design a beam that can carry a nervous

193

mini-elephant. The weight of the elephant is (the last two digits of your ID#/100) plus 1 kg.



Assume that the acceleration of gravity is 10 m/s2 and each leg carries the same amount of



gravitational force. The density of the beam is 5 x 10-5 kg/mm3. The beam width is 10 mm and



Young’s modulus is 100 N/mm2. He is so nervous that the free end of the beam should not deflect



more than 10 mm. What is the required beam depth, h? Check your results using GOYA-C.



x





h w



Deflection 20 20 60 mm

10 mm



Fig. 2-8-15



Hint: You may use the equation obtained in Example 2-8-5. You will have to solve a cubic



equation for the beam depth, h. Because the equation ( h3  ah2  bh  c  0 ) is difficult to solve



directly, you may resort to the following scheme: input y  h3  ah2  bh  c into a spreadsheet



and gradually increase h until you determine a deflection not exceeding 10 mm.









194

What is unit curvature?



Master, I could not understand the concept of



unit curvature.









OK. Imagine a circle which approximates the



beam axis. Unit curvature is the reciprocal of



the radius of the circle. A large curvature means a small



radius, which means that the top of the beam shortens



and the bottom lengthens considerably.









Another important point is M = EI, which indicates that the unit curvature is



proportional to the bending moment. You need more moment to bend more.









The equation,  = M/EI, also has an important meaning. An oak tree is hard to bend



because it has a high value of Young’s modulus. A thick board is also hard to bend



because it has large moment of inertia.









Yes, the wood I used in Chapter 1 bent very easily. But why are you so stiff when you are



so slim?









Cough! Anyhow, unit curvature has another face: it is the second derivative of the







195

deflection with respect to distance,  = d2v/dx2, which leads to the most important equation.



d 2v M



dx 2 EI



Integrating the bending moment, the beam deflection can be determined by calculation.







Unit curvature represents how a beam is bent, and the beam deflects because of the unit



curvature. It sounds circular. By the way, I don’t like calculus. It’s boring. Could you tell



me how to understand the idea intuitively?









Good question. In fact, calculus is rarely required



in most structural design. Engineering intuition is



much more important than calculus. The point is that a beam



will be concave upward under positive bending moment and



vice versa. You also need to train yourself so that you can



image how the beam will deflect. Solve the problems in the



next section and look at the graphics carefully in order to



develop a good intuition.









196



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