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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.

10.22
10.22.c
10.23
10.23.c
Step-by-Step
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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 RC 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
\quad\quad\quad\quad R_{A}+R_{B} {=}-R_{C}\quad\quad(a)
Sum moments about B (again using a statics sign convention in which counterclockwise is positive) to find
\quad\quad\quad\quad -R_{A}L+R_{C}a=0
so
\quad\quad\quad\quad R_{A}=\left({\frac{a}{L}}\right)R_{C}(b)
which can be subsitituted back into Eq. (a) to give
\quad\quad\quad\quad R_{B}=-R_{C}-{\Bigg\lgroup}{\frac{\alpha}{L}}{\Bigg\rgroup}R_{C}=-R_{C}{\Bigg\lgroup}1+{\frac{\alpha}{L}}{\Bigg\rgroup}\quad\quad (c)
(Note that you could also find reactions R_{A1} ~ and ~ R_{B1} 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
\quad\quad\quad\quad \delta_{C1}+\delta_{C2}=\delta_{C}=0\quad\quad (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,
\quad\quad\quad\quad \delta_{C1}={\frac{\alpha(T_{2}-T_{1})\alpha(L+a)}{2h}}\quad\quad (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),
\quad\quad\quad\quad \delta_{C2}={\frac{R_{C}a^{2}(L+\alpha)}{3E I}}\quad\quad (f)
Reactions: Now substitute Eqs. (e) and (f) into Eq. (d) and then solve for redundant R_C:
\quad\quad\quad\quad{\frac{\alpha(T_{2}-T_{1})}{2h_{-}}}(a)(L+a)+{\frac{R_{C}a^{2}(L+a)}{3E l}}= {0}
so
\quad\quad\quad\quad R_{C}={\frac{-3E I\alpha(T_{2}-T_{1})}{2\alpha h}}\quad\quad (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

\quad\quad\quad\quad R_{A}={\Bigg\lgroup}{\frac{\alpha}{L}}{\Bigg\rgroup}R_{C}={\Bigg\lgroup}{\frac{\alpha}{L}}{\Bigg\rgroup}\left[{\frac{-3EI\alpha(T_{2}-T_{1})}{2d h}}\right] = \frac{-3EI\alpha(T_{2}-T_{1})}{2L h}\quad\quad(h)
\begin{array}{cc} \quad\quad\quad\quad R_{B}=-{R}_{C}{\Bigg\lgroup}{1+{\frac{\alpha}{{L}}}}{\Bigg\rgroup}={\frac{3{E}{I}\alpha({T}_{2} – {T}_{1})}{2\alpha h}}{\Bigg\lgroup}{{1+{\cfrac{\alpha}{{L}}}}}{\Bigg\rgroup} \\ \quad\quad\quad\quad= \frac{3{E}{I}\alpha({T}_{2} – {T}_{1})(L + \alpha)}{2L\alpha h} \end{array} \quad (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, HE 700B (see Table F-1), with a length L = 9 m, an overhang a = L/2, and subject to temperature differential (T_2 – T_1) = 3°C. From Table I-4, the coefficient of thermal expansion for structural steel is a = 12 \times 10^{-6}/°C.
The modulus for steel is 210 GPa. Now find numerical values of reactions R_A, R_B, ~ and ~ R_C using Eqs. (g), (h), and (i):
\quad\quad\quad\quad R_A = \frac{- 3{E}{I}\alpha({T}_{2} – {T}_{1})}{2Lh} = \frac{-3(210~GPa)(256900~ cm^4)(12 \times 10^{-6})(3)}{2(9 ~M)(700 ~mm)} \\ \quad\quad\quad\quad = -4.62 kN (downward) \\ \quad\quad\quad\quad R_B = \frac{ 3{E}{I}\alpha({T}_{2} – {T}_{1})(L + \alpha)}{2L\alpha h} \\ \quad\quad\quad\quad\frac{3(210~GPa)(256900~ cm^4)(12 \times 10^{-6})(3)(9~m + 4.5~m)}{2(9 ~M)(4.5~m)(700 ~mm)} \\ \quad\quad\quad\quad = 13.87 kN ~(upward) \\ \quad\quad\quad\quad R_C = \frac{- 3{E}{L}\alpha({T}_{2} – {T}_{1})}{2\alpha h} = \frac{-3(210~GPa)(256900~ cm^4)(12 \times 10^{-6})(3)}{2(4.5 ~M)(700 ~mm)} \\ \quad\quad\quad\quad = -9.25 kN (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:
\quad\quad\quad\quad \delta_{1}+\delta_{2}= \delta =0\quad\quad (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
\quad\quad\quad\quad \delta_{2}={\frac{R_{C}}{k}}\,+\,\delta_{C2}\,=\,{\frac{R_{C}}{k}}\,+\,{\frac{R_{C}a^{2}(L\,+\,a)}{3E I}}\quad \quad(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:
\quad\quad\quad\quad \frac{\alpha(T_{2}-T_{1})}{2h}(a)(L+a)+\frac{{R}_{C}a^{2}(L+a)}{3E I}+\frac{{R}_{C}}{k}=0
so
\quad\quad\quad\quad R_{C}=\frac{-a\alpha(T_{2}-T_{1})(L+a)}{2h\left[\frac1k+\frac{a^{2}(L+a)}{3E I}\right]},\quad\quad(l)
From statics [Eqs. (b) and (c)], reactions at A and B are
\quad\quad\quad\quad R_{A} = {\Bigg\lgroup}\frac{a}{{L}}{\Bigg\rgroup}{R}_{C} = \frac{-\alpha\alpha(T_{2}-T_{1})\alpha(L+a)}{2Lh\left[\frac1k+\frac{a^{2}(L+a)}{3E I}\right]}\quad\quad(m)
\quad\quad\quad\quad R_{B} = -{R}_{C} {\Bigg\lgroup}1 + \frac{a}{{L}}{\Bigg\rgroup} = \frac{\alpha\alpha(T_{2}-T_{1})(L+a)^2}{2Lh\left[\frac1k+\frac{a^{2}(L+a)}{3E I}\right]}\quad\quad(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
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_f I_1 S_1 r_1 I_2 S_2 r_2
kg/m cm² mm mm mm mm cm⁴ cm³ cm cm⁴ cm³ cm
HE 1000 B 314 400 1000 300 19 36 644700 12890 40.15 16280 1085 6.38
HE 900 B 291 371.3 900 300 18.5 35 494100 10980 36.48 15820 1054 6.53
HE 700 B 241 306.4 700 300 17 32 256900 7340 28.96 14440 962.7 6.87
HE 650 B 225 286.3 650 300 16 31 210600 6480 27.12 13980 932.3 6.99
HE 600 B 212 270 600 300 15.5 30 171000 5701 25.17 13530 902 7.08
HE 550 B 199 254.1 550 300 15 29 136700 4971 23.2 13080 871.8 7.17
HE 600 A 178 226.5 590 300 13 25 141200 4787 24.97 11270 751.4 7.05
HE 450 B 171 218 450 300 14 26 79890 3551 19.14 11720 781.4 7.33
HE 550 A 166 211.8 540 300 12.5 24 111900 4146 22.99 10820 721.3 7.15
HE 360 B 142 180.6 360 300 12.5 22.5 43190 2400 15.46 10140 676.1 7.49
HE 450 A 140 178 440 300 11.5 21 63720 2896 18.92 9465 631 7.29
HE 340 B 134 170.9 340 300 12 21.5 36660 2156 14.65 9690 646 7.53
HE 320 B 127 161.3 320 300 11.5 20.5 30820 1926 13.82 9239 615.9 7.57
HE 360 A 112 142.8 350 300 10 17.5 33090 1891 15.22 7887 525.8 7.43
HE 340 A 105 133.5 330 300 9.5 16.5 27690 1678 14.4 7436 495.7 7.46
HE 320 A 97.6 124.4 310 300 9 15.5 22930 1479 13.58 6985 465.7 7.49
HE 260 B 93 118.4 260 260 10 17.5 14920 1148 11.22 5135 395 6.58
HE 240 B 83.2 106 240 240 10 17 11260 938.3 10.31 3923 326.9 6.08
HE 280 A 76.4 97.26 270 280 8 13 13670 1013 11.86 4763 340.2 7
HE 220 B 71.5 91.04 220 220 9.5 16 8091 735.5 9.43 2843 258.5 5.59
HE 260 A 68.2 86.82 250 260 7.5 12.5 10450 836.4 10.97 3668 282.1 6.5
HE 240 A 60.3 76.84 230 240 7.5 12 7763 675.1 10.05 2769 230.7 6
HE 180 B 51.2 65.25 180 180 8.5 14 3831 425.7 7.66 1363 151.4 4.57
HE 160 B 42.6 54.25 160 160 8 13 2492 311.5 6.78 889.2 111.2 4.05
HE 140 B 33.7 42.96 140 140 7 12 1509 215.6 5.93 549.7 78.52 3.58
HE 120 B 26.7 34.01 120 120 6.5 11 864.4 144.1 5.04 317.5 52.92 3.06
HE 140 A 24.7 31.42 133 140 5.5 8.5 1033 155.4 5.73 389.3 55.62 3.52
HE 100 B 20.4 26.04 100 100 6 10 449.5 89.91 4.16 167.3 33.45 2.53
HE 100 A 16.7 21.24 96 100 5 8 349.2 72.76 4.06 133.8 26.76 2.51
Table I-4
Coefficients of Thermal Expansion
Material Coefficient of
Thermal Expansion a
Material Coefficient of
Thermal Expansion a
10^{-6}/°C 10^{-6}/°C
Aluminum alloys 23 Plastics
Brass 19.1-21.2 Nylon 70–140
Bronze 18-21 Polyethylene 140–290
Cast iron 9.9-12 Rock 5–9
Concrete 7-14 Rubber 130–200
Copper and copper alloys 16.6-17.6 Steel 10–18
Glass 5–11 High-strength 14
Magnesium alloys 26.1-28.8 Stainless 17
Monel (67% Ni, 30% Cu) 14 Structural 12
Nickel 13 Titanium alloys 8.1–11
Tungsten 4.3

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