Solutions for Mechanics of Materials
Problem 1.1PP:
In each case, explain how to find the resultant internal loading acting on the cross section at...Problem 1.1FP:
Determine the resultant internal normal force, shear force, and bending moment at point C in the...Problem 1.2FP:
Determine the resultant internal normal force, shear force, and bending moment at point C in the...Problem 1.3FP:
Determine the resultant internal normal force, shear force, and bending moment at point C in the...Problem 1.4FP:
Determine the resultant internal normal force, shear force, and bending moment at point C in the...Problem 1.5FP:
Determine the resultant internal normal force, shear force, and bending moment at point C in the...Problem 1.6FP:
Determine the resultant internal normal force, shear force, and bending moment at point C in the...Problem 1.1P:
The shaft is supported by a smooth thrust bearing at B and a journal bearing at C. Determine the...Problem 1.2P:
Determine the resultant internal normal and shear force in the member at (a) section aa and (b)...Problem 1.3P:
1-3. The beam AB is fixed to the wall and has a uniform weight of 80 lb/ft. If the trolley supports...Problem 1.4P:
The shaft is supported by a smooth thrust bearing at A and a smooth journal bearing at B. Determine...Problem 1.5P:
1-5. Determine the resultant internal loadings in the beam at cross sections through points D and E....Problem 1.6P:
1-6. Determine the normal force, shear force, and moment at a section through point C. Take P = 8...Problem 1.7P:
1-7. The cable will fail when subjected to a tension of 2 kN. Determine the largest vertical load P...Problem 1.8P:
*1-8. Determine the resultant internal loadings on the cross section through point C. Assume the...Problem 1.9P:
1-9. Determine the resultant internal loadings on the cross section through point D. Assume the...Problem 1.10P:
The boom DF of the jib crane and the column DE have a uniform weight of 50 lb/ft. If the supported...Problem 1.11P:
1-11. The forearm and biceps support the 2-kg load at A. If C can be assumed as a pin support,...Problem 1.12P:
*1-12. The serving tray T used on an airplane is supported on each side by an arm. The tray is pin...Problem 1.13P:
The blade of the hacksaw is subjected to a pretension force of F= 100 N. Determine the resultant...Problem 1.14P:
The blade of the hacksaw is subjected to a pretension force of F= 100 N. Determine the resultant...Problem 1.15P:
1-15. A 150-lb bucket is suspended from a cable on the wooden frame. Determine the resultant...Problem 1.16P:
*1-16. A 150-lb bucket is suspended from a cable on the wooden frame. Determine the resultant...Problem 1.17P:
1-17. Determine resultant internal loadings acting on section a-a and section b-b. Each section...Problem 1.22P:
The metal stud punch is subjected to a force of 120 N on the handle. Determine the magnitude of the...Problem 1.23P:
Determine the resultant internal loadings acting on the cross section at point E of the handle arm,...Problem 1.25P:
1-25. Determine the resultant internal loading acting on the cross section through point B of the...Problem 1.26P:
1-26. The shaft is supported at its ends by two bearings A and B and is subjected to the forces...Problem 1.27P:
1-27. The pipe assembly is subjected to a force of 600 N at B. Determine the resultant internal...Problem 1.28P:
If the drill bit jams when the brace is subjected to the forces shown, determine the resultant...Browse All Chapters of This Textbook
Chapter 1 - StressChapter 1.2 - Equilibrium Of A Deformable BodyChapter 1.5 - Average Shear StressChapter 1.7 - Limit State DesignChapter 2.2 - StrainChapter 3 - Mechanical Properties Of MaterialsChapter 3.5 - Strain EnergyChapter 3.8 - Failure Of Materials Due To Creep And FatigueChapter 4 - Axial LoadChapter 4.2 - Elastic Deformation Of An Axially Loaded Member
Chapter 4.5 - The Force Method Of Analysis For Axially Loaded MembersChapter 4.6 - Thermal StressChapter 4.9 - Residual StressChapter 5 - TorsionChapter 5.3 - Power TransmissionChapter 5.4 - Angle Of TwistChapter 5.5 - Statically Indeterminate Torque-loaded MembersChapter 5.7 - Thin-walled Tubes Having Closed Cross SectionsChapter 5.10 - Residual StressChapter 6 - BendingChapter 6.2 - Graphical Method For Constructing Shear And Moment DiagramsChapter 6.4 - The Flexure FormulaChapter 6.5 - Unsymmetric BendingChapter 6.9 - Stress ConcentrationsChapter 6.10 - Inelastic BendingChapter 7 - Transverse ShearChapter 7.2 - The Shear FormulaChapter 7.3 - Shear Flow In Built-up MemebersChapter 7.5 - Shear Center For Open Thin Walled MembersChapter 8 - Combined LoadingsChapter 8.1 - Thin-walled Pressure VesselsChapter 8.2 - State Of Stress Caused By Combined LoadingsChapter 9 - Stress TransformationChapter 9.3 - Principal Stresses And Maximum In-plane Shear StressChapter 9.4 - Mohr's Circle Plane-stressChapter 9.5 - Absolute Maximum Shear StressChapter 10 - Strain TransformationChapter 10.3 - Mohr's Circle Plane-strainChapter 10.5 - Strain RossettesChapter 10.6 - Material-property RelationshipsChapter 10.7 - Theories Of FailureChapter 11 - Design Of Beams And ShaftsChapter 11.2 - Prismatic Beam DesignChapter 11.4 - Shaft DesignChapter 12 - Deflection Beams And ShaftsChapter 12.2 - Slope And Displacement By IntegrationChapter 12.3 - Discontinuity FunctionsChapter 12.4 - Slope And Displacement By Moment Area MethodChapter 12.5 - Method Of SuperpositionChapter 12.7 - Statically Indeterminate Beams And Shafts-method Of IntegrationChapter 12.8 - Statically Indeterminate Beams And Shafts-moment Area MethodChapter 12.9 - Statically Indeterminate Beams And Shafts-method Of SuperpositionChapter 13 - Buckling Of ColumnsChapter 13.3 - Columns Having Various Types Of SupportsChapter 13.5 - Inelastic BucklingChapter 13.6 - Design Of Columns For Concentric LoadingChapter 13.7 - Design Of Columns For Eccentric LoadingChapter 14 - Energy MethodsChapter 14.2 - Elastic Strain Energy For Various Types Of LoadingChapter 14.3 - Conservation Of EnergyChapter 14.4 - Impact LoadingChapter 14.6 - Method Of Virtual Forces Applied To TrussesChapter 14.7 - Method Of Virtual Forces Applied To BeamsChapter 14.9 - Castigliano's Theorem Applied To TrussesChapter 14.10 - Castigliano's Theorem Applied To Beams
Book Details
For undergraduate Mechanics of Materials courses in Mechanical, Civil, and Aerospace Engineering departments. Containing Hibbeler’s hallmark student-oriented features, this text is in four-color with a photorealistic art program designed to help students visualize difficult concepts. A clear, concise writing style and more examples than any other text further contribute to students’ ability to master the material.
Sample Solutions for this Textbook
We offer sample solutions for Mechanics of Materials homework problems. See examples below:
Chapter 1, Problem 1.97RPChapter 3, Problem 3.35RPChapter 4, Problem 4.114RPChapter 5, Problem 5.143RPChapter 6, Problem 6.1CPChapter 7, Problem 7.71RPChapter 8, Problem 8.74RPGiven information: Rotation of the propeller is ω=15 rad/s . The engine develops the power of 900...Chapter 10, Problem 10.94RP
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