Mechanics Of Materials, Si Edition9th EditionRussell C Hibbeler Publisher: Pearson EducationISBN: 9789810694364
Mechanics Of Materials, Si Edition
Solutions for Mechanics Of Materials, Si Edition
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
Sample Solutions for this Textbook
We offer sample solutions for Mechanics Of Materials, Si Edition 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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