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.
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
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 |