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.


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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=0so
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}=0so
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):
= – 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}=0so
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 |