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.

10.22
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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=0

so

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}=0

so

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):

\begin{aligned}&R_{A}=\frac{-3 E l \alpha\left(T_{2}-T_{1}\right)}{2 L h}=\frac{-3(210 \mathrm{~GPa})\left(256900 \mathrm{~cm}^{4}\right)\left(12 \times 10^{-6} /{ }^{\circ} \mathrm{C}\right)\left(3^{\circ} \mathrm{C}\right)}{2(9 \mathrm{~m})(700 \mathrm{~mm})}\\&=-4.62 \mathrm{kN} \text { (downward) }\\&R_{B}=\frac{3 E l \alpha\left(T_{2}-T_{1}\right)(L+a)}{2 L a h}\\&=\frac{3(210 \mathrm{~GPa})\left(256900 \mathrm{~cm}^{4}\right)\left(12 \times 10^{-6}/° \mathrm{C}\right)\left(3^{\circ} \mathrm{C}\right)(9 \mathrm{~m}+4.5 \mathrm{~m})}{2(9 \mathrm{~m})(4.5 \mathrm{~m})(700 \mathrm{~mm})}\\&=13.87 \mathrm{kN} \text { (upward) }\\&R_{C}=\frac{-3 E l \alpha\left(T_{2}-T_{1}\right)}{2 a h}=\frac{-3(210 \mathrm{~GPa})\left(256900 \mathrm{~cm}^{4}\right)\left(12 \times 10^{-6} /° \mathrm{C}\right)\left(3^{\circ} \mathrm{C}\right)}{2(4.5 \mathrm{~m}) 700 \mathrm{~mm}}\\&=-9.25 \mathrm{~kN} \text { (downward) }\end{aligned}

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}:

\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), (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).

10.23

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