Question 10.7: The two-span beam ABC in Fig. 10-22 below has a pin support ...
The two-span beam ABC in Fig. 10-22 below has a pin support at A, a roller support at B, and either a roller or elastic spring support (spring constant k) at C. The beam has a height of h and is subjected to a temperature differ-ential with temperature T_{1} on its upper surface and T_{2} on its lower surface (see Fig. 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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(a) Roller support at C. This beam (Fig. 10-22a) is statically indeterminate to the first degree (see discussion in Example 10-3 solution). We select reac-tion R_{C} as the redundant which allows us 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 tem-perature differential). We will use the method of superposition, also known as the force or flexibility method, to find the solution.
Superposition. The superposition process is shown in the Figs. 10-22b and 10-22c in which redundant R_{C} is removed to produce a released (or statically determinate) structure. We first apply the “actual loads” [here, temperature differential (T_{2} – T_{1} )], and then we apply the redundant as a load to the second released structure.
Equilibrium. Summing forces in the y direction in Fig. 10-22a (using a statics sign convention in which forces in the positive y direction are positive), we find that
R_{A}+R_{B}=-R_{C} (a)
Summing moments about B (again using a statics sign convention in which counterclockwise is positive), we find
-R_{A} L+R_{C} a=0so
R_{\mathrm{A}}=\left(\frac{\mathrm{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 we could also find reactions RA and RB using superposition of the reactions shown in Figs. 10-22b and c, as follows: R_{A}=R_{A 1}+R_{A 2} and R_{B}=R_{B 1}+R_{B 2} , where R_{A 1} and R_{B 1} 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_{\mathrm{C1}} and \delta_{\mathrm{C2}} are shown in Figs. 10-22b and 10-22c for the released structures subject to temperature differential and applied redundant force R_{C}, respectively. Initially, \delta_{\mathrm{C1}} and \delta_{\mathrm{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. We can now use the results of Examples 9-5 and 9-19 to find displacements \delta_{\mathrm{C1}} and \delta_{\mathrm{C1}} . First, from Eq. (f) in Example 9-19, we see that
\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}:
\delta_{C 2}=\frac{R_{c} a^{2}(L+a)}{3 E l} (f)
Reactions. We can 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 l \alpha\left(T_{2}-T_{1}\right)}{2 a h} (g)
noting that the negative result means that reaction force R_{C} is down-ward [for positive temperature differential (T_{2} – T_{1} ) ]. The result for R_{C} is now substituted 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 l \alpha\left(T_{2}-T_{1}\right)}{2 a h}\right]=\frac{-3 E l \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 \text { El } \alpha\left(T_{2}-T_{1}\right)}{2 a h}\left(1+\frac{a}{L}\right) \\&=\frac{3 E l \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.
Numerical example. In Example 9-19, we computed the upward displace-ment at joint C [see Eq. (h), Example 9-19] assuming that beam ABC is a steel wide flange, HE 700b (see Table E-1a), with a length L = 9 m an overhang a = L/2 , and is subject to temperature differentia T_{2} – T_{1} = 3° Celsius. From Table H-4, the coefficient of therma expan- sion for structural steel is \alpha=12 \times 10^{-6}{ }^{\circ} \mathrm{C} . The modulus for steel is 210 GPa. Now we can find numerical values of reactions R_{A}, R_{B}, and R_{C} using Eqs. (g), (h), and (i):
We note that the reactions sum to zero as required for equilibrium.
TABLE E-1
Properties of European Wide-Flange Beams
Designation | Mass per meter |
Area of section |
Depth of section |
Width of section |
Thickness | Strong axis 1-1 | Weak axis 2-2 | |||||
G | A | h | b | t_{w} | t_{t} | I_{1} | S_{1} | r_{1} | I_{2} | S_{2} | r_{2} | |
Kg/m | {cm}^{2} | mm | mm | mm | mm | {cm}^{4} | {cm}^{3} | cm | {cm}^{4} | {cm}^{3} | cm | |
HE 1000 B HE 900 B HE 700 B HE 650 b HE 600 B |
314 291 241 225 212 |
400 371.3 306.4 286.3 270 |
1000 900 700 650 600 |
300 300 300 300 300 |
19 18.5 17 16 15.5 |
36 35 32 31 30 |
644700 494100 256900 210600 171000 |
12890 10980 7340 6480 5701 |
40.15 36.48 28.96 27.12 25.17 |
16280 15820 14440 13980 13530 |
1085 1054 962.7 932.3 902 |
6.38 6.53 6.87 6.99 7.08 |
HE 550 B HE 600 A HE 450 B HE 550 A HE 360 B HE 450 A |
199 178 171 166 142 140 |
254.1 226.5 218 211.8 180.6 178 |
550 590 450 540 360 440 |
300 300 300 300 300 300 |
15 13 14 12.5 12.5 11.5 |
29 25 26 24 22.5 21 |
136700 141200 79890 111900 43190 63720 |
4971 4787 3551 4146 2400 2896 |
23.2 24.97 19.14 22.99 15.46 18.92 |
13080 11270 11720 10820 10140 9465 |
871.8 751.4 781.4 721.3 676.1 631 |
7.17 7.05 7.33 7.15 7.49 7.29 |
HE 340 B HE 320 B HE 360 A HE 340 A |
134 127 112 105 |
170.9 161.3 142.8 133.5 |
340 320 350 330 |
300 300 300 300 |
12 11.5 10 9.5 |
21.5 20.5 17.5 16.5 |
36660 30820 33090 27690 |
2156 1926 1891 1678 |
14.65 13.82 15.22 14.4 |
9690 9239 7887 7436 |
646 615.9 525.8 495.7 |
7.53 7.57 7.43 7.46 |
HE 320 A HE 260 B HE 240 B HE 280 A HE 220 B HE 260 A HE 240 A |
97.6 93 83.2 76.4 71.5 68.2 60.3 |
124.4 118.4 106 97.26 91.04 86.82 76.84 |
310 260 240 270 220 250 230 |
300 260 240 280 220 260 240 |
9 10 10 8 9.5 7.5 7.5 |
15.5 17.5 17 13 16 12.5 12 |
22930 14920 11260 13670 8091 10450 7763 |
1479 1148 938.3 1013 735.5 836.4 675.1 |
13.58 11.22 10.31 11.86 9.43 10.97 10.05 |
6985 5135 3923 4763 2843 3668 2769 |
465.7 395 326.9 340.2 258.5 282.1 230.7 |
7.49 6.58 6.08 7 5.59 6.5 6 |
HE 180 B HE 160 B HE 140 B HE 120 B HE 140 A |
51.2 42.6 33.7 26.7 24.7 |
65.25 54.25 42.96 34.01 31.42 |
180 160 140 120 133 |
180 160 140 120 140 |
8.5 8 7 6.5 5.5 |
14 13 12 11 8.5 |
3831 2492 1509 864.4 1033 |
425.7 311.5 215.6 144.1 155.4 |
7.66 6.78 5.93 5.04 5.73 |
1363 889.2 549.7 317.5 389.3 |
151.4 111.2 78.52 52.92 55.62 |
4.57 4.05 3.58 3.06 3.52 |
HE 100 B HE 100 A |
20.4 16.7 |
26.4 21.24 |
100 96 |
100 100 |
6 5 |
10 8 |
449.5 349.2 |
89.91 72.76 |
4.16 4.06 |
167.3 133.8 |
33.45 26.76 |
2.53 2.51 |
Note: Axes 1-1 and 2-2 are principal centroidal axes. |
Table H-4
Coefficients of Thermal Expansion
Material | Coefficient of thermal expansion α |
10^{-6}/°C | |
Aluminum alloys | 23 |
Brass | 19.1-21.2 |
Bronze | 18-21 |
Cast iron | 9.9-21 |
Concrete | 7-14 |
Copper and copper alloys | 16.6–17.6 |
Glass | 5-11 |
Magnesium alloys | 26.1-28.8 |
Monel (67% Ni, 30% Cu) | 14 |
Nickel | 13 |
Plastics Nylon Polethylene |
70-140 140-290 |
Rock | 5-9 |
Rubber | 130-200 |
Steel High-strength Stainless Structural |
10-18 14 17 12 |
Titanium alloys | 8.1-11 |
Tungsten | 4.3 |
(b) Spring support at C. Once again, we select reaction R_{C} as the redundant. However, R_{C} is now at the base of the elastic spring support. When redundant reaction R_{C} is applied to the second released structure, it will first compress the spring and then be applied to the beam at C, causing upward deflection.
Superposition. The superposition solution approach (i.e., force or flexi-bility method) follows that used previously and is shown in Fig. 10-23.
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, we see that compatibility of displacements requires:
\delta_{1}+\delta_{2}=\delta=0 (i)
Force-displacement and temperature-displacement relations. The spring is assumed to be unaffected by the differential change, so we conclude that 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_{C 1} . However, we must include the compression of the spring in the expression for \delta_{2}, so we get
\delta_{2}=\frac{R_{C}}{k}+\delta_{C}=\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. We can now substitute Eqs. (e) and (k) into compatibility with Eq. (j) and then solve for redundant R_{C}:
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), (c)], we find:
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)
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).
