Question 10.7: The two-span beam ABC in Fig. 10-22 has a pin support at A, ...

The two-span beam ABC in Fig. 10-22 has a pin support at A, a roller support at B, and either a roller (Fig. 10-22) or elastic spring support (Fig. 10-23) (spring constant k) at C. The beam has a height of h and is subjected to a temperature differential with temperature T_{1} on its upper surface and T_{2} on its lower surface (see Figs. 10-22a and b). Assume that the elastic spring is unaffected by the temperature change.

(a) If support C is a roller support, find all support reactions using the method of superposition.

(b) Find all support reactions if the roller at C is replaced by the elastic spring support; also find the displacement at C.

10.7
10..7
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Use a four-step problem-solving approach.
Part (a): Roller support at C.
1. Conceptualize:
Roller support at C: This beam (Fig. 10-22a) is statically indeterminate to the first degree (see discussion in Example 10-3 solution). Select reaction R_{C} as the redundant in order to use the analyses of the released structure (with the support at C removed) presented in Examples 9-5 (concentrated load applied at C) and 9-19 (subject to temperature differential). Use the method of superposition, also known as the force or flexibility method, to find the solution.

2. Categorize:
Superposition: The superposition process is shown in the Figs. 10-22b and c in which redundant R_{C} is removed to produce a released (or statically determinate) structure.

First apply the “actual loads” [here, temperature differential (T_{2} – T_{1}) ], and then apply the redundant R_{C} as a load to the second released structure.

3. Analyze:
Equilibrium: Sum forces in the y direction in Fig. 10-22a (using a statics sign convention in which upward forces in the y direction are positive) to find that

R_{A}+R_{B}=-R_{C}             (a)

Sum moments about B (again using a statics sign convention in which counterclockwise is positive) to find

-R_{A} L+R_{C} a=0

so

R_{A}=\left(\frac{a}{L}\right) R_{C}            (b)

which can be subsitituted back into Eq. (a) to give

R_{B}=-R_{C}-\left(\frac{a}{L}\right) R_{C}=-R_{C}\left(1+\frac{a}{L}\right)              (c)

(Note that you could also find reactions R_{A}  and  R_{B} using superposition of the reactions shown in Figs. 10-22b and c: R_{A} = R_{A1} + R_{A2}  and  R_{B} = R_{B1} + R_{B2}, where R_{A1}  and  R_{B1} are known to be zero.)

Compatibility: Displacement \delta_{C} = 0 in the actual structure (Fig. 10-22a), so compatibility of displacements requires that

\delta_{C 1}+\delta_{C 2}=\delta_{C}=0            (d)

where \delta_{C1}  and  \delta_{C2} are shown in Figs. 10-22b and c for the released structures subject to temperature differential and applied redundant force R_{C}, respectively. Initially, \delta_{C1}  and  \delta_{C2} are assumed positive (upward) when using a statics sign convention, and a negative result indicates that the reverse is true.

Force-displacement and temperature-displacement relations: Now use the results of Examples 9-5 and 9-19 to find displacements \delta_{C1}  and  \delta_{C2}. First, from Eq. (f) in Example 9-19,

\delta_{C 1}=\frac{\alpha\left(T_{2}-T_{1}\right) a(L+a)}{2 h}           (e)

and from Eq. (9-55) (modified to include variable a as the length of member BC and replacing load P with redundant force R_{C} – see solution to Problems 9.8-5(b) or 9.9-3),

\delta_{C}=-v\left(\frac{3 L}{2}\right)=\frac{P L^{3}}{8 E I}              (9-55)

\delta_{C 2}=\frac{R_{C} a^{2}(L+a)}{3 E I}             (f)

Reactions: Now substitute Eqs. (e) and (f) into Eq. (d) and then solve for redundant R_{C}:

\frac{\alpha\left(T_{2}-T_{1}\right)}{2 h}(a)(L+a)+\frac{R_{ C } a^{2}(L+a)}{3 E I}=0

so

R_{C}=\frac{-3 E I \alpha\left(T_{2}-T_{1}\right)}{2 a h}               (g)

noting that the negative result means that reaction force R_{C} is downward [for positive temperature differential (T_{2} – T_{1})]. Now substitute the expression for R_{C} into Eqs. (b) and (c) to find reactions R_{A} and R_{B} as

R_{A}=\left(\frac{a}{L}\right) R_{C}=\left(\frac{a}{L}\right)\left[\frac{-3 E I \alpha\left(T_{2}-T_{1}\right)}{2 a h}\right]=\frac{-3 E I \alpha\left(T_{2}-T_{1}\right)}{2 L h}             (h)

\begin{aligned}R_{B} &=-R_{C}\left(1+\frac{a}{L}\right)=\frac{3 E I \alpha\left(T_{2}-T_{1}\right)}{2 a h}\left(1+\frac{a}{L}\right) \\&=\frac{3 E I \alpha\left(T_{2}-T_{1}\right)(L+a)}{2 L a h}\end{aligned}             (i)

where R_{A} acts downward and R_{B} acts upward.

4. Finalize:
Numerical example: In Example 9-19, the upward displacement at joint C was computed [see Eq. (h), Example 9-19] assuming that beam ABC is a steel wide flange, W 30 × 211 (see Table F-1a), with a length L = 30 ft, an overhang a = L/2, and subject to temperature differential (T_{2} – T_{1}) =  5°F. From Table I-4, the coefficient of thermal expansion for structural steel is \alpha = 6.5 \times 10^{-6} /°F . The modulus for steel is 30,000 ksi. Now find numerical values of reactions R_{A}, R_{B}, and R_{C} using Eqs. (g), (h), and (i):

R_{A}=\frac{-3 E I \alpha\left(T_{2}-T_{1}\right)}{2 L h}=\frac{-3(30,000  ksi )\left(10,300  in ^{4}\right)\left(6.5 \times 10^{-6}\right)(5)}{2(360  in .)(30  in .)}

= – 1.395 kips (downward)

R_{B}=\frac{3 E I \alpha\left(T_{2}-T_{1}\right)(L+a)}{2 L a h}

= \frac{3(30,000  ksi )\left(10,300  in ^{4}\right)\left(6.5 \times 10^{-6}\right)(5)(360  in .+180  in .)}{2(360  in .)(180  in .)(30  in .)}

= 4.18 kips (upward)

R_{C}=\frac{-3 E L \alpha\left(T_{2}-T_{1}\right)}{2 a h}=\frac{-3(30,000  ksi )\left(10,300  in ^{4}\right)\left(6.5 \times 10^{-6}\right)(5)}{2(180  in .) 30  in .}

= – 2.79 kips (downward)

Note that the reactions sum to zero as required for equilibrium.

Part (b): Elastic spring support at C.

1. Conceptualize:
Spring support at C: Once again, select reaction R_{C} as the redundant. However, R_{C} is now at the base of the elastic spring support (see Fig. 10-23). When redundant reaction R_{C} is applied to the second released structure (Fig. 10-23c), it will first compress the spring and then be applied to the beam at C, causing upward deflection.
2. Categorize:
Superposition: The superposition solution approach (i.e., force or flexibility method) follows that used previously and is shown in Fig. 10-23.
3. Analyze:
Equilibrium: The addition of the spring support at C does not alter the expressions of static equilibrium in Eqs. (a), (b), and (c).

Compatibility: The compatibility equation is now written for the base of the spring (not the top of the spring, where it is attached to the beam at C). From Fig. 10-23, compatibility of displacements requires:

\delta_{1}+\delta_{2}=\delta=0          (j)

Force-displacement and temperature-displacement relations: The spring is assumed to be unaffected by the temperature differential, so the top and base of the spring displace the same in Fig. 10-23b, which means that Eq. (e) is still valid and \delta_{1} = \delta_{C1}. However, the compression of the spring must be included in the expression for \delta_{2}, so

\delta_{2}=\frac{R_{C}}{k}+\delta_{C 2}=\frac{R_{C}}{k}+\frac{R_{C} a^{2}(L+a)}{3 E I}          (k)

where the expression for \delta_{C2} comes from Eq. (f).

Reactions: Now substitute Eqs. (e) and (k) into compatibility with Eq. (j) and solve for redundant R_{C}:

\frac{\alpha\left(T_{2}-T_{1}\right)}{2 h}(a)(L+a)+\frac{R_{C} a^{2}(L+a)}{3 E I}+\frac{R_{C}}{k}=0

so

R_{C}=\frac{-a \alpha\left(T_{2}-T_{1}\right)(L+a)}{2 h\left[\frac{1}{k}+\frac{a^{2}(L+a)}{3 E I}\right]}            (l)

From statics [Eqs. (b) and (c)], reactions at A and B are

R_{A}=\left(\frac{a}{L}\right) R_{C}=\frac{-a \alpha\left(T_{2}-T_{1}\right) a(L+a)}{2 L h\left[\frac{1}{k}+\frac{a^{2}(L+a)}{3 E I}\right]}              (m)

R_{B}=-R_{C}\left(1+\frac{a}{L}\right)=\frac{a \alpha\left(T_{2}-T_{1}\right)(L+a)^{2}}{2 L h\left[\frac{1}{k}+\frac{a^{2}(L+a)}{3 E I}\right]}          (n)

4. Finalize: Once again, the minus signs for R_{A}  and  R_{C} indicate that they are downward [for positive (T_{2} – T_{1})], while R_{B} is upward. Finally, if spring constant k goes to infinity, the support at C is once again a roller support, as in Fig. 10-22, and Eqs. (l), (m), and (n) reduce to Eqs. (g), (h), and (i).

Table F-1(a)
Properties of Wide-Flange Sections (W Shapes)—USCS Units (Abridged List)
Designation Weight
per
Foot
Area Depth Web
Thickness
Flange Axis 1–1 Axis 2-2
Width Thickness I S r I S r
lb in² in. in. in. in. \text{in}^{4} in³ in. \text{in}^{4} in³ in.
W 30 × 211 211 62.2 30.9 0.775 15.1 1.32 10300 665 12.9 757 100 3.49
W 30 × 132 132 38.9 30.3 0.615 10.5 1.00 5770 380 12.2 196 37.2 2.25
W 24 × 162 162 47.7 25.0 0.705 13.0 1.22 5170 414 10.4 443 68.4 3.05
W 24 × 94 94.0 27.7 24.3 0.515 9.07 0.875 2700 222 9.87 109 24.0 1.98
W 18 × 119 119 35.1 19.0 0.655 11.3 1.06 2190 231 7.90 253 44.9 2.69
W 18 × 71 71.0 20.8 18.5 0.495 7.64 0.810 1170 127 7.50 60.3 15.8 1.70
W 16 × 100 100 29.5 17.0 0.585 10.4 0.985 1490 175 7.10 186 35.7 2.51
W 16 × 77 77.0 22.6 16.5 0.455 10.3 0.760 1110 134 7.00 138 26.9 2.47
W 16 × 57 57.0 16.8 16.4 0.430 7.12 0.715 758 92.2 6.72 43.1 12.1 1.60
W 16 × 31 31.0 9.13 15.9 0.275 5.53 0.440 375 47.2 6.41 12.4 4.49 1.17
W 14 × 120 120 35.3 14.5 0.590 14.7 0.940 1380 190 6.24 495 67.5 3.74
W 14 × 82 82.0 24.0 14.3 0.510 10.1 0.855 881 123 6.05 148 29.3 2.48
W 14 × 53 53.0 15.6 13.9 0.370 8.06 0.660 541 77.8 5.89 57.7 14.3 1.92
W 14 × 26 26.0 7.69 13.9 0.255 5.03 0.420 245 35.3 5.65 8.91 3.55 1.08
W  12 × 87 87.0 25.6 12.5 0.515 12.1 0.810 740 118 5.38 241 39.7 3.07
W 12 × 50 50.0 14.6 12.2 0.370 8.08 0.640 391 64.2 5.18 56.3 13.9 1.96
W 12 × 35 35.0 10.3 12.5 0.300 6.56 0.520 285 45.6 5.25 24.5 7.47 1.54
W 12 × 14 14.0 4.16 11.9 0.200 3.97 0.225 88.6 14.9 4.62 2.36 1.19 0.753
W 10 × 60 60.0 17.6 10.2 0.420 10.1 0.680 341 66.7 4.39 116 23.0 2.57
W 10 × 45 45.0 13.3 10.1 0.350 8.02 0.620 248 49.1 4.32 53.4 13.3 2.01
W 10 × 30 30.0 8.84 10.5 0.300 5.81 0.510 170 32.4 4.38 16.7 5.75 1.37
W 10× 12 12.0 3.54 9.87 0.190 3.96 0.210 53.8 10.9 3.90 2.18 1.10 0.785
W 8 × 35 35.0 10.3 8.12 0.310 8.02 0.495 127 31.2 3.51 42.6 10.6 2.03
W 8 × 28 28.0 8.24 8.06 0.285 6.54 0.465 98.0 24.3 3.45 21.7 6.63 1.62
W 8 × 21 21.0 6.16 8.28 0.250 5.27 0.400 75.3 18.2 3.49 9,77 3.71 1.26
W 8 × 15 15.0 4.44 8.11 0.245 4.01 0.315 48.0 11.8 3.29 3.41 1.70 0.876

 

TABLE I-4
Coefficients of Thermal Expansion
Material Coefficient of
Thermal expansion α
10^{-6} /{ }^{\circ} F 10^{-6} /^{\circ} C
Aluminum alloys 13 23
Brass 10.6–11.8 19.1–21.2
Bronze 9.9–11.6 18–21
Cast iron 5.5–6.6 9.9–12
Concrete 4–8 7–14
Copper and copper alloys 9.2–9.8 16.6–17.6
Glass 3–6 5–11
Magnesium alloys 14.5–16.0 26.1–28.8
Monel (67% Ni, 30% Cu) 7.7 14
Nickel 7.2 13
Plastics

Nylon

Polyethylene

 

40–80

80–160

 

70–140

140–290

Rock 3-5 5-9
Rubber 70–110 130–200
Steel
High-strength
Stainless
Structural
5.5–9.9
8.0
9.6
6.5
10–18
14
17
12
Titanium alloys 4.5–6.0 8.1–11
Tungsten 2.4 4.3

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