7/21/2019 Mechanics of Materials Solutions Chapter11 Probs18 25 http://slidepdf.com/reader/full/mechanics-of-materials-solutions-chapter11-probs18-25 1/13 Excerpts from this work may be reproduced by instructors for distribution on a not-for-profit basis for testing or instructional purposes only to students enrolled in courses for which the textbook has been adopted. Any other reproduction or translation of this work beyond that permitted by Sections 107 or 108 of the 1976 United States Copyright Act without the permission of the copyright owner is unlawful.11.18a For the beams and loadings shown below, assume that EI = 3.0 × 10 4 kN-m 2 is constant for each beam. (a) For the beam in Fig. P11.18a, determine the concentrated upward force P required to make the total beam deflection at B equal to zero (i.e., v B = 0). Fig. P11.18aSolution Downward deflection at B due to 15 kN/m uniformly distributed load. [Appendix C, SS beam with uniformly distributed load over portion of span.] Relevant equation from Appendix C: 3 2 2 (4 7 3 ) 24 B wa v L aL a LEI = − − + Values:w = 15 kN/m, L = 7 m, a = 3.5 m, EI = 3.0 × 10 4 kN-m 2 Computation: 3 2 2 3 3 2 2 (4 7 3 ) 24 (15 kN/m)(3.5 m) 234.472656 kN-m 4(7 m) 7(3.5 m)(7 m) 3(3.5 m) 24(7 m) B wa v L aL a LEI EI EI = − − + ⎡ ⎤ = − − + = − ⎣ ⎦ Upward deflection at B due to concentrated load P . [Appendix C, SS beam with concentrated load at midspan.] Relevant equation from Appendix C: 3 48 B PL v EI = Values: L = 7 m, EI = 3.0 × 10 4 kN-m 2 Computation: 3 3 3 (7 m) (7.145833 m) 48 48 B PL P P v EI EI EI = = = Compatibility equation at B: 3 3 3 3 234.472656 kN-m (7.145833 m ) 0 234.472656 kN-m 32.8125 kN 32.8 kN 7.145833 m P EI EI P − + = ∴ = = = Ans.
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7/21/2019 Mechanics of Materials Solutions Chapter11 Probs18 25
Excerpts from this work may be reproduced by instructors for distribution on a not-for-profit basis for testing or instructional purposes onlyto students enrolled in courses for which the textbook has been adopted. Any other reproduction or translation of this work beyond that
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11.18a For the beams and loadings shown below, assume that EI = 3.0 × 10
4 kN-m
2is
constant for each beam.
(a) For the beam in Fig. P11.18a, determine
the concentrated upward force P required tomake the total beam deflection at B equal to
zero (i.e., v B = 0).
Fig. P11.18a
Solution
Downward deflection at B due to 15 kN/m uniformly distributed load.
[Appendix C, SS beam with uniformly distributed load over portion of span.]
Relevant equation from Appendix C:3
2 2(4 7 3 )24
B
wav L aL a
LEI = − − +
Values: w = 15 kN/m, L = 7 m, a = 3.5 m,
EI = 3.0 × 104
kN-m2
Computation:3
2 2
3 32 2
(4 7 3 )24
(15 kN/m)(3.5 m) 234.472656 kN-m4(7 m) 7(3.5 m)(7 m) 3(3.5 m)
24(7 m)
B
wav L aL a
LEI
EI EI
= − − +
⎡ ⎤= − − + = −⎣ ⎦
Upward deflection at B due to concentrated load P .
[Appendix C, SS beam with concentrated load at midspan.]
Relevant equation from Appendix C:3
48 B
PLv
EI =
Values: L = 7 m, EI = 3.0 × 10
4 kN-m
2
Computation:3 3 3(7 m) (7.145833 m )
48 48 B
PL P P v
EI EI EI = = =
Compatibility equation at B:3 3
3
3
234.472656 kN-m (7.145833 m )0
234.472656 kN-m32.8125 kN 32.8 kN
7.145833 m
P
EI EI
P
− + =
∴ = = = Ans.
7/21/2019 Mechanics of Materials Solutions Chapter11 Probs18 25
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11.18b For the beams and loadings shown below, assume that EI = 3.0 × 10
4 kN-m
2is
constant for each beam.
(b) For the beam in Fig. P11.18b, determinethe concentrated moment M required to
make the total beam slope at A equal to zero
(i.e., θ A = 0).
Fig. P11.18b
Solution
Slope at A due to 32 kN concentrated load.
[Appendix C, Cantilever beam with concentrated load at tip.]
Relevant equation from Appendix C:2
2 A
PL
EI θ = (slope magnitude)
Values: P = 32 kN, L = 4 m, EI = 3.0 × 10
4 kN-m
2
Computation:2 2 2(32 kN)(4 m) 256 kN-m
(negative slope by inspection)2 2
A
PL
EI EI EI θ = = = −
Slope at A due to concentrated moment M .
[Appendix C, Cantilever beam with concentrated moment at tip.]
Relevant equation from Appendix C:
A L EI
θ = (slope magnitude)
Values: L = 4 m, EI = 3.0 × 10
4 kN-m
2
Computation:
(4 m) (4 m)(positive slope by inspection) A
ML M M
EI EI EI θ = = =
Compatibility equation at A:2
2
256 kN-m (4 m)0
256 kN-m64.0 kN-m
4 m
M
EI EI
M
− + =
∴ = = Ans.
7/21/2019 Mechanics of Materials Solutions Chapter11 Probs18 25
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11.19a For the beams and loadings shown below, assume that EI = 5.0 × 10
6 kip-in.
2is
constant for each beam.
(a) For the beam in Fig. P11.19a, determinethe concentrated upward force P required to
make the total beam deflection at B equal to
zero (i.e., v B = 0).
Fig. P11.19a
Solution
Downward deflection at B due to 4 kips/ft uniformly distributed load.
[Appendix C, Cantilever beam with uniformly distributed load.]
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11.19b For the beams and loadings shown below, assume that EI = 5.0 × 10
6 kip-in.
2is
constant for each beam.
(b) For the beam in Fig. P11.19b, determinethe concentrated moment M required to
make the total beam slope at C equal to zero
(i.e., θ C = 0).
Fig. P11.19b
Solution
Slope at C due to 40-kip concentrated load.
[Appendix C, SS beam with concentrated load at midspan.]
Relevant equation from Appendix C:2
16C
PL
EI θ = (slope magnitude)
Values: P = 40 kips, L = 18 ft, EI = 5.0 × 10
6 kip-in.
2
Computation:2 2 2(40 kips)(18 ft) 810 kip-ft
(negative slope by inspection)16 16
C
PL
EI EI EI θ = = =
Slope at C due to concentrated moment M .
[Appendix C, SS beam with concentrated moment at one end.]
Relevant equation from Appendix C:
3
C
L
EI
θ = (slope magnitude)
Values: L = 18 ft, EI = 5.0 × 10
6 kip-in.
2
Computation:
(18 ft) (6 ft)(positive slope by inspection)
3 3C
ML M M
EI EI EI θ = = =
Compatibility equation at C :2
2
810 kip-ft (6 ft)0
810 kip-ft135.0 kip-ft
6 ft
M
EI EI
M
− + =
∴ = = Ans.
7/21/2019 Mechanics of Materials Solutions Chapter11 Probs18 25
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11.20a For the beams and loadings shown below, assume that EI = 5.0 × 10
4 kN-m
2
is constant for each beam.
(a) For the beam in Fig. P11.20a,
determine the concentrated downwardforce P required to make the total beam
deflection at B equal to zero (i.e., v B = 0).
Fig. P11.20a
Solution
Upward deflection at B due to 105 kN-m concentrated moment.
[Appendix C, SS beam with concentrated moment at one end.]
Relevant equation from Appendix C:
2 2(2 3 )6
B
M xv L Lx x
LEI = − − + (elastic curve)
Values: M = −105 kN-m, L = 8 m, x = 4 m,
EI = 5.0 × 104 kN-m
2
Computation:
2 2
32 2
(2 3 )6
( 105 kN-m)(4 m) 420 kN-m2(8 m) 3(8 m)(4 m) (4 m)
6(8 m)
B
M xv L Lx x
LEI
EI EI
= − − +
−⎡ ⎤= − − + =⎣ ⎦
Downward deflection at B due to concentrated load P .
[Appendix C, SS beam with concentrated load at midspan.]
Relevant equation from Appendix C:3
48 B
PLv
EI = −
Values: L = 8 m, EI = 5.0 × 10
4 kN-m
2
Computation:3 3 3(8 m) (10.666667 m )
48 48 B
PL P P v
EI EI EI = − = − = −
Compatibility equation at B:3 3
3
3
420 kN-m (10.666667 m )0
420 kN-m39.375 kN 39.4 kN
10.666667 m
P
EI EI
P
− =
∴ = = = Ans.
7/21/2019 Mechanics of Materials Solutions Chapter11 Probs18 25
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11.20b For the beams and loadings shown below, assume that EI = 5.0 × 10
4 kN-m
2is
constant for each beam.
(b) For the beam in Fig. P11.20b, determinethe concentrated moment M required to
make the total beam slope at A equal to zero
(i.e., θ A = 0).
Fig. P11.20b
Solution
Slope at A due to 6 kN/m uniformly distributed load.
[Appendix C, Cantilever beam with uniformly distributed load.]
Relevant equation from Appendix C:3
6 A
wL
EI θ = (slope magnitude)
Values: w = 6 kN/m, L = 5 m, EI = 5.0 × 10
4 kN-m
2
Computation:3 3 2(6 kN/m)(5 m) 125 kN-m
(positive slope by inspection)6 6
A
wL
EI EI EI θ = = =
Slope at A due to concentrated moment M .
[Appendix C, Cantilever beam with concentrated moment at tip.]
Relevant equation from Appendix C:
A
L
EI θ = (slope magnitude)
Values: L = 5 m, EI = 5.0 × 10
4 kN-m
2
Computation:
(5 m)(negative slope by inspection) A
ML M
EI EI θ = =
Compatibility equation at A:2
2
125 kN-m (5 m)0
125 kN-m25.0 kN-m
5 m
M
EI EI
M
− =
∴ = = Ans.
7/21/2019 Mechanics of Materials Solutions Chapter11 Probs18 25
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11.21a For the beams and loadings shown below, assume that EI = 8.0 × 10
6 kip-in.
2
is constant for each beam.
(a) For the beam in Fig. P11.21a,determine the concentrated downward
force P required to make the total beam
deflection at B equal to zero (i.e., v B = 0).
Fig. P11.21a
Solution
Upward deflection at B due to 125 kip-ft concentrated moment.
[Appendix C, Cantilever beam with concentrated moment at tip.]
Excerpts from this work may be reproduced by instructors for distribution on a not-for-profit basis for testing or instructional purposes onlyto students enrolled in courses for which the textbook has been adopted. Any other reproduction or translation of this work beyond that
permitted by Sections 107 or 108 of the 1976 United States Copyright Act without the permission of the copyright owner is unlawful.
11.21b For the beams and loadings shown below, assume that EI = 8.0 × 10
6 kip-in.
2
is constant for each beam.
(b) For the beam in Fig. P11.21b,determine the concentrated moment
required to make the total beam slope at A
equal to zero (i.e., θ A = 0).
Fig. P11.21b
Solution
Slope at A due to 7 kips/ft uniformly distributed load.
[Appendix C, SS beam with uniformly distributed load over portion of span.]
Relevant equation from Appendix C:2
2 2(2 )24
A
wa L a
LEI θ = − (slope magnitude)
Values: w = 7 kips/ft, L = 23 ft, a = 15 ft,
EI = 8.0 × 106 kip-in.
2
Computation:2
2 2
22 2
2
(2 )24
(7 kips/ft)(15 ft)2(23 ft) (15 ft)
24(23 ft)
2,376.766304 kip-ft(negative slope by inspection)
A
wa L a
LEI
EI
EI
θ = −
⎡ ⎤= −⎣ ⎦
= −
Slope at A due to concentrated moment M .[Appendix C, SS beam with concentrated moment at one end.]
Relevant equation from Appendix C:
3 A
L
EI θ = (slope magnitude)
Values: L = 23 ft, EI = 8.0 × 10
6 kip-in.
2
Computation:
(23 ft) (7.666667 ft)(positive slope by inspection)
3 3 A
ML M M
EI EI EI θ = = =
Compatibility equation at A:2
2
2,376.766304 kip-ft (7.666667 ft)0
2,376.766304 kip-ft310 kip-ft
7.666667 ft
M
EI EI
M
− + =
∴ = = Ans.
7/21/2019 Mechanics of Materials Solutions Chapter11 Probs18 25
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11.22 For the beam and loading shown below, derive an expression for the reactions
at supports A and B. Assume that EI is
constant for the beam.
Fig. P11.22
Solution
Choose the reaction force at B as the redundant; therefore, the released beam is a cantilever.
Consider downward deflection of cantilever beam at B due to concentrated moment M 0.
[Appendix C, Cantilever beam with concentrated moment at tip.]
Relevant equation from Appendix C:2 2
0
2 2 B
L M Lv
EI EI = − = −
Consider upward deflection of cantilever beam at B due to concentrated load R B.
[Appendix C, Cantilever beam with concentrated load at tip.]
Relevant equation from Appendix C:3 3
3 3
B B
PL R Lv
EI EI = =
Compatibility equation for deflection at B:2 3
0 030
2 3 2
B B
M L R L M R
EI EI L− + = ∴ = ↑ Ans.
Equilibrium equations
for entire beam:
0 03 30
2 2 y A B A B
M M F R R R R
L LΣ = + = ∴ = − = − = ↓ Ans.
0 0 A A B M M M R LΣ = − − + =
0 0 00 0 0
3 3( ) (cw)
2 2 2 A B
M M M M R L M L M M
L∴ = − = − = − = Ans.
7/21/2019 Mechanics of Materials Solutions Chapter11 Probs18 25
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11.23 For the beam and loading shown below, derive an expression for the reactions
at supports A and B. Assume that EI is
constant for the beam.
Fig. P11.23
Solution
Choose the reaction force at B as the redundant; therefore, the released beam is a cantilever.
Consider downward deflection of cantilever beam at B due to linearly distributed load.
[Appendix C, Cantilever beam with linearly distributed load.]
Relevant equation from Appendix C:4
0
30 B
w Lv
EI = −
Consider upward deflection of cantilever beam at B due to concentrated load R B.
[Appendix C, Cantilever beam with concentrated load at tip.]
Relevant equation from Appendix C:3 3
3 3
B B
PL R Lv
EI EI = =
Compatibility equation for deflection at B:4 3
0 0030 3 10
B B
w L R L w L R
EI EI − + = ∴ = ↑ Ans.
Equilibrium equations for entire beam:
0 0 0 0 04 20
2 2 10 10 5
y A B A
w L w L w L w L w L F R R RΣ = + − = ∴ = − = = ↑ Ans.
0 02 3
A A B
w L L M M R L
⎛ ⎞Σ = − − + =⎜ ⎟
⎝ ⎠
2 2 2 2
0 0 0 0 0( ) (ccw)6 10 6 15 15
A B
w L w L w L w L w L M R L L∴ = − = − = − = Ans.
7/21/2019 Mechanics of Materials Solutions Chapter11 Probs18 25
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permitted by Sections 107 or 108 of the 1976 United States Copyright Act without the permission of the copyright owner is unlawful.
11.24 For the beam and loading shown below,derive an expression for the reactions at
supports A and B. Assume that EI is constant
for the beam.
Fig. P11.24
Solution
Choose the reaction force at A as the redundant; therefore, the released beam is a cantilever.
Consider downward deflection of cantilever beam at A due to concentrated load P .
[Appendix C, Cantilever beam with concentrated load at tip.]
Relevant equation from Appendix C:2
(3 )6
A
Pxv L x
EI = − − (elastic curve)
2 3
3Let ,2
( ) 3 73
6 2 12 A
L x L L
P L L PLv L
EI EI
= =
⎡ ⎤⎛ ⎞∴ = − − = −⎜ ⎟⎢ ⎥
⎝ ⎠⎣ ⎦
Consider upward deflection of cantilever beam at A due to concentrated load R A.
[Appendix C, Cantilever beam with concentrated load at tip.]
Relevant equation from Appendix C:3 3
3 3
A A
PL R Lv
EI EI = =
Compatibility equation for deflection at A:
3 37 70
12 3 4
A A
PL R L P R
EI EI − + = ∴ = ↑ Ans.
Equilibrium equations for entire beam:
0
7 3 34 4 4
y A B
B
F R R P
P P P R P
Σ = + − =
∴ = − = − = ↓ Ans.
3
02
B B A
L M M R L P
⎛ ⎞Σ = − + =⎜ ⎟
⎝ ⎠
3 7 3( ) (ccw)
2 4 2 4 4 B A
L P PL PL PL M R L P L
⎛ ⎞∴ = − = − = =⎜ ⎟
⎝ ⎠ Ans.
7/21/2019 Mechanics of Materials Solutions Chapter11 Probs18 25
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11.25 For the beam and loading shown below,derive an expression for the reactions at
supports A and B. Assume that EI is constant
for the beam.
Fig. P11.25
Solution
Choose the reaction force at A as the redundant; therefore, the released beam is a cantilever.
Consider downward deflection of cantilever beam at A due to uniformly distributed load.
[Appendix C, Cantilever beam with uniformly distributed load.]
Relevant equation from Appendix C:2
2 2(6 4 )24
A
wxv L Lx x
EI = − − + (elastic curve)
22 42
3Let ,
2
( ) 3 3 176 4 ( ) ( )
24 2 2 48 A
L x L L
w L L L wLv L L
EI EI
= =
⎡ ⎤⎛ ⎞ ⎛ ⎞∴ = − − + = −⎢ ⎥⎜ ⎟ ⎜ ⎟
⎝ ⎠ ⎝ ⎠⎢ ⎥⎣ ⎦
Consider upward deflection of cantilever beam at A due to concentrated load R A.
[Appendix C, Cantilever beam with concentrated load at tip.]
Relevant equation from Appendix C:3 3
3 3
A A
PL R Lv
EI EI = =
Compatibility equation for deflection at A:4 317 17
048 3 16
A A
wL R L wL R
EI EI − + = ∴ = ↑ Ans.
7/21/2019 Mechanics of Materials Solutions Chapter11 Probs18 25
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