(Book Solutions) Structural Analysis by R C Hibbeler(Ninth Edition)

The book ‘Structural Analysis’ by R C Hibbeler is followed worldwide in various engineering colleges. Each Unsolved Problem in this book has a unique number, and hence the chapter name and the problem numbers are given below. Choose the problem solution by referring to its number as given in the book.

Other Books Solutions:

Book Title: Mechanics of Materials, Author: R C Hibbeler (Eighth Edition)

Chapter 4: Internal Loadings Developed in Structural Members

Fundamental Problems

F4-1 Solution ( R C Hibbeler, Structural Analysis)

F4-4 Solution (R C Hibbeler, Structural Analysis)

F4-5 Solution (R C Hibbeler, Structural Analysis)

F4-6 Solution (R C Hibbeler, Structural Analysis)

F4-7 Solution (R C Hibbeler, Structural Analysis)

F4-8 Solution (R C Hibbeler, Structural Analysis)

F4-9 Solution (R C Hibbeler, Structural Analysis)

F4-10 Solution (R C Hibbeler, Structural Analysis)

F4-11 Solution (R C Hibbeler, Structural Analysis)

F4-12 Solution (R C Hibbeler, Structural Analysis)

F4-13 Solution (R C Hibbeler, Structural Analysis)

F4-14 Solution (R C Hibbeler, Structural Analysis)

F4-17 Solution (R C Hibbeler, Structural Analysis)

F4-18 Solution (R C Hibbeler, Structural Analysis)

F4-20 Solution (R C Hibbeler, Structural Analysis)

PROBLEMS:

4-6 Solution (chapter -4, R C Hibbeler, Structural Analysis)

4-7 Solution (chapter -4, R C Hibbeler, Structural Analysis)

4-9 Solution (chapter -4, R C Hibbeler, Structural Analysis)

4-10 Solution (chapter -4, R C Hibbeler, Structural Analysis)

Chapter 5: Cables and Arches

Section: PROBLEMS.

Problem 5-1. (Solution) Calculate the tension in each segment of the cable and also find out the distance YD. ( R C Hibbeler.)

Problem 5-2. (Solution) The Cable supports the loading shown. Determine the distance xB the force at B acts from A. Set P = 200 N. ( R C Hibbeler.)

Problem 5-3. (Solution) Determine the Forces P1 and P2 needed so that the segment BC of the cable remains horizontal. [Problem 5-3. Structural Analysis by R C Hibbeler.]

Problem 5-4. (Solution) Determine the tension in each segment of the cable and the cable’s total length. Set P = 400 N.[Problem 5-4. Structural Analysis by R C Hibbeler.]

Problem 5-6. (Solution) Cable ABCD supports the loading shown. Determine the maximum tension in the cable and the sag of point B.[Problem 5-6. Structural Analysis by R C Hibbeler.]

Problem 5-7. (Solution) The cable supports the three loads shown. Determine the magnitude of P1 if P2 = 3 kN and yB = 0.8m. Also, find the sag yD.[Problem 5-7. Structural Analysis by R C Hibbeler.]

Chapter 6: Influence Lines for Statically Determinate Structures

PROBLEMS (Problem 6-1 to Problem 6-10)

Problem 6-1. (Solution) Sketch the influence line diagram for (a) the vertical reaction at A, (b) the shear at B, and (c) the moment at B. Assume A is fixed.[Problem 6-1. Structural Analysis by R C Hibbeler.]

Problem 6-3. (Solution) Sketch the influence line diagram for (a) the vertical reaction at A, (b) the shear at C, and (c) the moment at C. [Problem 6-3. Structural Analysis by R C Hibbeler.]

Problem 6-5. (Solution) Draw the influence line diagram for (a) the vertical reaction at B, (b) the shear just to the right of the rocket at A, and (c) the moment at C.[Problem 6-5. Structural Analysis by R C Hibbeler.]

Problem 6-7. (Solution) Draw the influence line diagram for (a) the moment at B, (b) the shear at C, and (c) the vertical reaction at B. Solve this problem using the basic method. [Problem 6-7. Structural Analysis by R C Hibbeler.]

Problem 6-9. (Solution) Draw the influence line diagram for (a) the vertical reaction at A, (b) the shear at C, and (c) the Moment at C. Solve this problem using the basic method. Assume A is a roller, and B is a pin. [ Prob 6-9. Chapter – 6, Structural Analysis by R C Hibbeler]

PROBLEMS (Problem 6-11 to Problem 6-20)

Problem 6-11. (Solution) Draw the influence line diagram for (a) the vertical reaction at B, (b) the shear just to the left of B,(c) the Moment at B. Solve this problem using the basic method. [ Prob 6-11. Chapter – 6, Structural Analysis by R C Hibbeler]

Problem 6-13. (Solution) Draw the influence line diagram for (a) the Moment at C,(b) the Shear just to the right of , and (c) the vertical reaction at B. Solve this problem using the basic method. Assume A is a pin, and B is a roller. [ Prob 6-13. Chapter – 6, Structural Analysis by R C Hibbeler]

Problem 6-15.(Solution) The beam is subjected to a uniform dead load of 3 kN/m and a concentrated live load of 60 kN. Determine (a) the maximum moment created by these loads at C, and (b) the maximum positive shear at C. Assume A is a pin, and B is a roller. [ Prob 6-15. chapter – 6, Structural Analysis by R C Hibbeler]

Problem 6-16.(Solution) A uniform live load of 10 kN/m and a single concentrated force of 120 kN are to be subjected on the beam. Determine (a) the maximum positive live vertical reaction at support B, (b) the maximum positive live shear at point C, and (c) the maximum positive live moment at point C.[ Prob 6-16. chapter – 6, Structural Analysis by R C Hibbeler]

Problem 6-17.(Solution) A uniform live load of 4 kN/m and a single concentrated force of 6 kN are placed on the beam. The beam has a weight of 2 kN/m. Determine (a) the maximum vertical reaction at support B, (b) the maximum negative moment at point B.[ Prob 6-17. chapter – 6, Structural Analysis by R C Hibbeler]

Problem 6-20.(Solution) The Compound Beam is subjected to a uniformly distributed dead load of 3 kN/m and a single concentrated live load of 40 kN.[ Prob 6-20. chapter – 6, Structural Analysis by R C Hibbeler]

PROBLEMS (Problem 6-21 to Problem 6-25)

Problem 6-21.(Solution) For the largest moment at D, a single 5 -kN-m live load should be placed on the beam at a distance from the point C? Find out this moment?[ Prob 6-21. chapter – 6, Structural Analysis by R C Hibbeler]

Problem 6-22.(Solution) The beam is subjected to a uniform live load of 5 kN/m, a dead load of 2 kN/m, and a single live load of 80 kN. Determine (a) the maximum positive moment at E..[ Prob 6-22. chapter – 6, Structural Analysis by R C Hibbeler]

Problem 6-23.(Solution) The beam supports a distributive dead load of 600 N/m and a single live concentrated force of 500 N. Determine (a) the maximum negative moment at E, and (b) the maximum positive shear at E. [ Prob 6-23. chapter – 6, Structural Analysis by R C Hibbeler]

Problem 6-24‘s (Solution) The beam is subjected to a dead load of 10 kN/m, a live load of 80 kN/m, and a concentrated live load of 60 kN. Determine (a) the maximum positive vertical reaction at A,[ Prob 6-24. chapter – 6, Structural Analysis by R C Hibbeler]

Problem 6-25‘s (Solution) Draw the Influence Line for (a) the vertical reaction at A, (b) the shear just to the right of B, and (c) the moment at A. Assume A is fixed, C is roller, and B is a pin.[ Prob 6-25. chapter – 6, Structural Analysis by R C Hibbeler]

Chapter 14:

Truss Analysis Using the Stiffness Method

PROBLEMS (Problem 14-1 to Problem 14-12)

Problem 14-1 Assuming all joints are pin-connected, determine the stiffness matrix K for the truss. Take A = 500 mm², E = 200 GPa.

Problem 14-2. Determine the Vertical Deflection of joint 1 and the force in member 2 of the truss in problem 14-1.

Problem 14-3, Determine the Stiffness Matrix K for the truss. Take A = 0.0015 m² and E = 200 GPa for each member.

Problem 14-4, Determine the vertical deflection at joint 2 and the force in member 4 of the truss in prob. 14-3. Take A = 0.0015 m² and E = 200 GPa for each member.

Problem 14-5, Determine the Stiffness Matrix K for the truss. Take A = 0.0015 m2 and E = 200 GPa for each member.