Hibbeler Mechanics of Materials 10th Edition Instructors Solution Manual Chapter 1 Solutions PDF

Title Hibbeler Mechanics of Materials 10th Edition Instructors Solution Manual Chapter 1 Solutions
Author Luis Alvarez
Course Mechanics of Materials
Institution University of South Florida
Pages 104
File Size 6 MB
File Type PDF
Total Downloads 17
Total Views 148

Summary

Here is the Instructor's Solution Manual to learn the procedures of analysis to solve a variety of problems explored in Mechanics of Materials/Mechanics of Solids....


Description

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1–1. The shaft is supported by a smooth thrust bearing atB and a journal bearing at C. Determine the resultant internal loadings acting on the cross section at E.

B

A

4 ft

C

E

4 ft

4 ft

D

4 ft

400 lb 800 lb

SOLUTION Support Reactions: We will only need to compute Cy by writing the moment equation of equilibrium about B with reference to the free-body diagram of the entire shaft, Fig. a. a+ Σ MB = 0;

Cy(8) + 400(4) - 800(12) = 0

Cy = 1000 lb

Internal Loadings: Using the result for Cy, section DE of the shaft will be considered. Referring to the free-body diagram, Fig. b, + Σ Fx = 0; S Fy = 0; + cΣ

NE = 0

Ans.

VE + 1000 - 800 = 0

VE = -200 lb

Ans.

a+ Σ ME = 0; 1000(4) - 800(8) - ME = 0

ME = - 2400 lb # ft = - 2.40 kip # ft

Ans.

The negative signs indicates that VE and ME act in the opposite sense to that shown on the free-body diagram.

Ans: NE = 0, VE = -200 lb, ME = - 2.40 kip # ft 1

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1–2. Determine the resultant internal normal and shear force in the member at (a) section a–a and (b) section b–b, each of which passes through the centroid A. The 500-lb load is applied along the centroidal axis of the member.

a

b 30

500 lb

500 lb

A b

a

SOLUTION (a) + Fx = 0; SΣ

Na - 500 = 0 Na = 500 lb

Ans.

Fy = 0; +T Σ

Va = 0

Ans.

Fx = 0; R+ Σ

Nb - 500 cos 30° = 0

(b)

Nb = 433 lb +Q Σ Fy = 0;

Ans.

Vb - 500 sin 30° = 0 Vb = 250 lb

Ans.

Ans: (a) Na = 500 lb, Va = 0, (b) Nb = 433 lb, Vb = 250 lb 2

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1–3. Determine the resultant internal loadings acting on section b–b through the centroid C on the beam. B b

900 lb/ft

b

C

A

30

60 3 ft

6 ft

SOLUTION Support Reaction: a+ Σ MA = 0;

NB(9 sin 30°) -

1 (900)(9)(3) = 0 2

NB = 2700 lb Equations of Equilibrium: For section b–b + Σ Fx = 0; S

F +cΣ

y

= 0;

MC = 0; a+ Σ

1 (300)(3) sin 30° - 2700 = 0 2 Vb - b = 2475 lb = 2.475 kip

Ans.

1 (300)(3) cos 30° = 0 2 Nb - b = 389.7 lb = 0.390 kip

Ans.

Vb - b +

Nb - b -

2700(3 sin 30°) -

1 (300)(3)(1) - Mb - b = 0 2

Mb - b = 3600 lb # ft = 3.60 kip # ft

Ans.

Ans: Vb - b = 2.475 kip, Nb - b = 0.390 kip, Mb - b = 3.60 kip # ft 3

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*1–4. The shaft is supported by a smooth thrust bearing atA and a smooth journal bearing at B. Determine the resultant internal loadings acting on the cross section at C.

600 N/m A

D

B C

1m

1m

1m

1.5 m

1.5 m 900 N

SOLUTION Support Reactions: We will only need to compute By by writing the moment equation of equilibrium about A with reference to the free-body diagram of the entire shaft, Fig. a. a+ Σ MA = 0;

B y(4.5) - 600(2)(2) - 900(6) = 0

B y = 1733.33 N

Internal Loadings: Using the result of By, section CD of the shaft will be considered. Referring to the free-body diagram of this part, Fig. b, + Σ Fx = 0; S F +c Σ

y

= 0;

a+ Σ MC = 0;

NC = 0 VC - 600(1) + 1733.33 - 900 = 0

Ans. VC = -233 N

Ans.

1733.33(2.5) - 600(1)(0.5) - 900(4) - MC = 0

MC = 433 N # m

Ans.

The negative sign indicates that VC acts in the opposite sense to that shown on the free-body diagram.

Ans: NC = 0, VC = -233 N, MC = 433 N # m 4

© 2017 Pearson Education, Inc., Hoboken, NJ. All rights reserved. This material is protected under all copyright laws as they currently exist. No portion of this material may be reproduced, in any form or by any means, without permission in writing from the publisher.

1–5. Determine the resultant internal loadings acting on the cross section at point B.

60 lb/ ft

A

C

B 3 ft

12 ft

SOLUTION + Σ Fx = 0; S F +c Σ

y

= 0;

NB = 0 VB -

Ans.

1 (48)(12) = 0 2

VB = 288 lb a+ Σ MB = 0;

-MB -

Ans.

1 (48)(12)(4) = 0 2

MB = -1152 lb # ft = -1.15 kip # ft

Ans.

Ans: NB = 0, VB = 288 lb, MB = -1.15 kip # ft 5

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1–6. Determine the resultant internal loadings on the cross section at point D.

C

1m

F

2m

1.25 kN/m

SOLUTION

A

Support Reactions: Member BC is the two force member. 4 a+ Σ MA = 0; F (1.5) - 1.875(0.75) = 0 5 BC

D

E

0.5 m 0.5 m 0.5 m

B

1.5 m

FBC = 1.1719 kN F +cΣ

y

= 0;

Ay +

4 (1.1719) - 1.875 = 0 5

Ay = 0.9375 kN + Σ Fx = 0; S

3 (1.1719) - Ax = 0 5 Ax = 0.7031 kN

Equations of Equilibrium: For point D + Σ Fx = 0; S Fy = 0; +cΣ a+ Σ MD = 0;

ND - 0.7031 = 0 ND = 0.703 kN

Ans.

0.9375 - 0.625 - VD = 0 VD = 0.3125 kN

Ans.

MD + 0.625(0.25) - 0.9375(0.5) = 0 MD = 0.3125 kN # m

Ans.

Ans: ND = 0.703 kN , VD = 0.3125 kN , MD = 0.3125 kN # m 6

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1–7. Determine the resultant internal loadings at cross sections at points E and F on the assembly.

C

1m

F

2m

1.25 kN/m

SOLUTION

A

Support Reactions: Member BC is the two-force member. 4 a+ Σ F (1.5) - 1.875(0.75) = 0 MA = 0; 5 BC

D

E

0.5 m 0.5 m 0.5 m

B

1.5 m

FBC = 1.1719 kN Fy = 0; +cΣ

Ay +

4 (1.1719) - 1.875 = 0 5

Ay = 0.9375 kN + Σ Fx = 0; S

3 (1.1719) - Ax = 0 5 Ax = 0.7031 kN

Equations of Equilibrium: For point F + bΣ Fx′ = 0;

NF - 1.1719 = 0 NF = 1.17 kN

Ans.

a+Σ Fy′ = 0;

VF = 0

Ans.

MF = 0; a+ Σ

MF = 0

Ans.

Equations of Equilibrium: For point E 3 +Σ Fx = 0; NE - (1.1719) = 0 d 5 NE = 0.703 kN Fy = 0; +cΣ

VE - 0.625 +

Ans.

4 (1.1719) = 0 5

VE = -0.3125 kN a+ Σ ME = 0;

-ME - 0.625(0.25) +

Ans. 4 (1.1719)(0.5) = 0 5

ME = 0.3125 kN # m

Ans.

Negative sign indicates that VE acts in the opposite direction to that shown on FBD.

Ans: NF = 1.17 kN, VF = 0, MF = 0, NE = 0.703 kN, VE = -0.3125 kN, ME = 0.3125 kN # m 7

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*1–8. The beam supports the distributed load shown. Determine the resultant internal loadings acting on the cross section at point C. Assume the reactions at the supports A and B are vertical.

4 kN/m

A

B C 1.5 m

D 3m

1.5 m

SOLUTION Support Reactions: Referring to the FBD of the entire beam, Fig. a, a+ Σ MA = 0;

By(6) -

1 (4)(6)(2) = 0 2

By = 4.00 kN

Internal Loadings: Referring to the FBD of the right segment of the beam sectioned through C, Fig. b, + Σ Fx = 0; S

NC = 0

Fy = 0; +cΣ

VC + 4.00 -

MC = 0; a+ Σ

4.00(4.5) -

Ans. 1 (3)(4.5) = 0 2

VC = 2.75 kN

Ans.

1 (3)(4.5)(1.5) - MC = 0 2

MC = 7.875 kN # m

Ans.

Ans: NC = 0 , VC = 2.75 kN , MC = 7.875 kN # m 8

© 2017 Pearson Education, Inc., Hoboken, NJ. All rights reserved. This material is protected under all copyright laws as they currently exist. No portion of this material may be reproduced, in any form or by any means, without permission in writing from the publisher.

1–9. The beam supports the distributed load shown. Determine the resultant internal loadings acting on the cross section at point D. Assume the reactions at the supports A and B are vertical.

4 kN/m

A

B C 1.5 m

D 3m

1.5 m

SOLUTION Support Reactions: Referring to the FBD of the entire beam, Fig. a, a+ Σ MA = 0;

B y(6) -

1 (4)(6)(2) = 0 2

By = 4.00 kN

Internal Loadings: Referring to the FBD of the right segment of the beam sectioned through D, Fig. b, + Σ Fx = 0; S

ND = 0

Ans.

Fy = 0; +c Σ

V D + 4.00 -

a+ Σ MD = 0;

4 .00(1.5) -

1 (1.00)(1.5) = 0 2

VD = -3.25 kN

Ans.

1 (1.00)(1.5)(0.5) - MD = 0 2

MD = 5.625 kN # m

Ans.

The negative sign indicates that VD acts in the sense opposite to that shown on the FBD.

Ans: ND = 0, VD = -3.25 kN, MD = 5.625 kN # m 9

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1–10. The boom DF of the jib crane and the column DE have a uniform weight of 50 lb>ft. If the supported load is 300 lb, determine the resultant internal loadings in the crane on cross sections at points A, B, and C.

D

B 2 ft

A 8 ft

F

3 ft

5 ft C 300 lb 7 ft

SOLUTION Equations of Equilibrium: For point A + Σ Fx = 0; d Fy = 0; +c Σ

E

NA = 0

Ans.

VA - 150 - 300 = 0 VA = 450 lb

a+ Σ MA = 0;

Ans.

-MA - 150(1.5) - 300(3) = 0

MA = -1125 lb # ft = -1.125 kip # ft

Ans.

Negative sign indicates that MA acts in the opposite direction to that shown on FBD. Equations of Equilibrium: For point B + Σ Fx = 0; d F +c Σ

y

= 0;

NB = 0

Ans.

VB - 550 - 300 = 0 VB = 850 lb

a+ Σ MB = 0;

Ans.

-MB - 550(5.5) - 300(11) = 0

MB = -6325 lb # ft = -6.325 kip # ft

Ans.

Negative sign indicates that MB acts in the opposite direction to that shown on FBD. Equations of Equilibrium: For point C + Σ Fx = 0; d Fy = 0; +c Σ

VC = 0

Ans.

-NC - 250 - 650 - 300 = 0 NC = -1200 lb = -1.20 kip

MC = 0; a+ Σ

Ans.

-MC - 650(6.5) - 300(13) = 0 MC = -8125 lb # ft = -8.125 kip # ft

Ans.

Negative signs indicate that NC and MC act in the opposite direction to that shown on FBD.

Ans: NA = 0, VA = 450 lb, MA = -1.125 kip # ft, NB = 0, VB = 850 lb,MB = -6.325 kip # ft, VC = 0, NC = -1.20 kip, MC = -8.125 kip # ft 10

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1–11. Determine the resultant internal loadings acting on the cross sections at points D and E of the frame.

C

1 ft F

4 ft

75 lb/ft A

1 ft

SOLUTION Member AG:

B 1 ft

E

G 2 ft

1 ft

30 150 lb

a+ Σ MA = 0;

4 F (3) - 75(4)(5) - 150 cos 30°(7) = 0; 5 BC

a+ Σ MB = 0;

Ay (3) - 75(4)(2) - 150 cos 30°(4) = 0; Ay = 373.20 lb

+ Σ Fx = 0; S

D 2 ft

Ax -

FBC = 1003.89 lb

3 (1003.89) + 150 sin 30° = 0; Ax = 527.33 l b 5

For point D: + Σ Fx = 0; S

ND + 527.33 = 0 ND = -527 lb

+cΣ Fy = 0;

Ans.

-373.20 - VD = 0 VD = -373 lb

MD = 0; a+ Σ

Ans.

MD + 373.20(1) = 0 MD = -373 lb # ft

Ans.

For point E: + Σ Fx = 0; S

150 sin 30° - NE = 0 NE = 75.0 lb

Fy = 0; +cΣ

Ans.

VE - 75(3) - 150 cos 30° = 0 VE = 355 lb

ME = 0; a+ Σ

Ans.

-ME - 75(3)(1.5) - 150 cos 30°(3) = 0; ME = -727 lb # ft

Ans.

Ans: ND = -527 lb, VD = -373 lb, MD = -373 lb # ft , NE = 75.0 lb, VE = 355 lb , ME = -727 lb # ft 11

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*1–12. Determine the resultant internal loadings acting on the cross sections at points F and G of the frame.

C

1 ft F

4 ft

75 lb/ft A

1 ft

SOLUTION Member AG: a+ Σ MA = 0;

D 2 ft

B 1 ft

E

G 2 ft

1 ft

30 150 lb

4 F (3) - 300(5) - 150 cos 30°(7) = 0 5 BF FBF = 1003.9 lb

For point F: +Q Σ Fx′ = 0; Fy′ = 0; a+Σ

a+ Σ MF = 0;

VF = 0

Ans.

NF - 1003.9 = 0 NF = 1004 lb

Ans.

MF = 0

Ans.

For point G: + Σ Fx = 0; d

NG - 150 sin 30° = 0 NG = 75.0 lb

Fy = 0; + cΣ

Ans.

VG - 75(1) - 150 cos 30° = 0 VG = 205 lb

MG = 0; a+ Σ

Ans.

-MG - 75(1)(0.5) - 150 cos 30°(1) = 0 MG = -167 lb # ft

Ans.

Ans: VF = 0, NF = 1004 lb, MF = 0 , NG = 75.0 lb , VG = 205 lb , MG = -167 lb # ft 12

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1–13. a

The blade of the hacksaw is subjected to a pretension force of F = 100 N. Determine the resultant internal loadings acting on section a–a that passes through point D.

225 mm 30 b B

A D b F E

150 mm a

F C

SOLUTION Internal Loadings: Referring to the free-body diagram of the section of the hacksaw shown in Fig. a, + Σ Fx = 0; d

Na - a + 100 = 0

Fy = 0; +cΣ

Va - a = 0

a+ Σ MD = 0;

- Ma - a - 100(0.15) = 0

Na - a = -100 N

Ans. Ans.

Ma - a = -15 N # m

Ans.

The negative sign indicates that N a - a and Ma - a act in the opposite sense to that shown on the free-body diagram.

Ans: Na - a = -100 N, Va - a = 0, Ma - a = -15 N # m 13

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1–14. a

The blade of the hacksaw is subjected to a pretension force of F = 100 N. Determine the resultant internal loadings acting on section b–b that passes through point D.

225 mm 30 b B

A D b F E

150 mm a

F C

SOLUTION Internal Loadings: Referring to the free-body diagram of the section of the hacksaw shown in Fig. a, Σ F

x′

= 0;

Nb - b + 100 cos 30° = 0

Nb - b = - 86.6 N

Ans.

Σ F

y′

= 0;

Vb - b - 100 sin 30° = 0

Vb - b = 50 N

Ans.

- Mb - b - 100(0.15) = 0

Mb - b = -15 N # m

Ans.

a+ Σ MD = 0;

The negative sign indicates that Nb–b and Mb–b act in the opposite sense to that shown on the free-body diagram.

Ans: Nb - b = - 86.6 N, Vb - b = 50 N , Mb - b = -15 N # m 14

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1–15. The beam supports the triangular distributed load shown. Determine the resultant internal loadings on the cross section at point C. Assume the reactions at the supports A and B are vertical.

800 lb/ft

A D 6 ft

6 ft

C 6 ft

B

E

4.5 ft 4.5 ft

SOLUTION Support Reactions: Referring to the FBD of the entire beam, Fig. a, a+ Σ MB = 0;

1 1 (0.8)(18)(6) - (0.8)(9)(3) - Ay(18) = 0 2 2

Ay = 1.80 kip

Internal Loadings: Referring to the FBD of the left beam segment sectioned through point C, Fig. b, + Σ Fx = 0; S

NC = 0

Fy = 0; +cΣ

1.80 -

MC = 0; a+ Σ

MC +

1 (0.5333)(12) - VC = 0 2

Ans. VC = -1.40 kip

...


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