Engineering Mechanics of Materials4. 2 Solid Circular Shafts-Angle of Twist and Shearing Stresses 159 4. 3 Hollow Circular Shafts-Angle of Twist and Shearing Stresses 166 4. 4 Principal Stresses and Strains Associated with Torsion 173 4. 5 Analytical and Experimental Solutions for Torsion of Members of Noncircular Cross Sections 179 4. 6 Shearing Stress-Strain Properties 188 *4. 7 Computer Applications 195 5 Stresses in Beams 198 5. 1 Introduction 198 5. 2 Review of Properties of Areas 198 5. 3 Flexural Stresses due to Symmetric Bending of Beams 211 5. 4 Shear Stresses in Symmetrically Loaded Beams 230 *5. 5 Flexural Stresses due to Unsymmetric Bending of Beams 248 *5. 6 Computer Applications 258 Deflections of Beams 265 I 6. 1 Introduction 265 6. 2 Moment-Curvature Relationship 266 6. 3 Beam Deflections-Two Successive Integrations 268 6. 4 Derivatives of the Elastic Curve Equation and Their Physical Significance 280 6. 5 Beam Deflections-The Method of Superposition 290 6. 6 Construction of Moment Diagrams by Cantilever Parts 299 6. 7 Beam Deflections-The Area-Moment Method 302 *6. 8 Beam Deflections-Singularity Functions 319 *6. 9 Beam Deflections-Castigliano's Second Theorem 324 *6. 10 Computer Applications 332 7 Combined Stresses and Theories of Failure 336 7. 1 Introduction 336 7. 2 Axial and Torsional Stresses 336 Axial and Flexural Stresses 342 7. 3 Torsional and Flexural Stresses 352 7. 4 7. 5 Torsional, Flexural, and Axial Stresses 358 *7. 6 Theories of Failure 365 Computer Applications 378 *7. |
From inside the book
Results 1-5 of 83
Page 10
... subjected to these gravity loadings . 50 k Roof 1.3 A 30 - ft - long vertical cable supports a weight of 5000 lb at its lower end . The cable weighs 4 lb / ft and is supported at its upper end . Determine the vertical sup- porting force ...
... subjected to these gravity loadings . 50 k Roof 1.3 A 30 - ft - long vertical cable supports a weight of 5000 lb at its lower end . The cable weighs 4 lb / ft and is supported at its upper end . Determine the vertical sup- porting force ...
Page 12
... subjected to two applied forces and each segment has unit weights as follows : wA = 10 lb / ft and WB = 5 lb / ft . Draw the appropriate free - body diagrams required to express the axial forces in this bar as func- tions of a length ...
... subjected to two applied forces and each segment has unit weights as follows : wA = 10 lb / ft and WB = 5 lb / ft . Draw the appropriate free - body diagrams required to express the axial forces in this bar as func- tions of a length ...
Page 18
... and fixed torsionally at its right end . It is subjected to variable torques as shown in Fig . 1.11 ( a ) . The intensities of these torsional loadings are given analytically by q = 5√x ( 0 ≤ x ≤ 4 ). 18 Ch . 1 Internal Forces in ...
... and fixed torsionally at its right end . It is subjected to variable torques as shown in Fig . 1.11 ( a ) . The intensities of these torsional loadings are given analytically by q = 5√x ( 0 ≤ x ≤ 4 ). 18 Ch . 1 Internal Forces in ...
Page 21
... subjected to the torques shown in Fig . P1.20 . These applied torques are resisted at D. Compute the reacting torque at D and draw the torque diagram for this shaft . 1.22 Draw the torque diagram for the shaft depicted in Fig . P1.22 ...
... subjected to the torques shown in Fig . P1.20 . These applied torques are resisted at D. Compute the reacting torque at D and draw the torque diagram for this shaft . 1.22 Draw the torque diagram for the shaft depicted in Fig . P1.22 ...
Page 22
... subjected to a torque of 40 k- in . at A and a uniformly distributed torque of 4 k - in / in . over its full length . These applied torques are resisted by a torsional reaction at B. Determine the internal torque T as a function of x ...
... subjected to a torque of 40 k- in . at A and a uniformly distributed torque of 4 k - in / in . over its full length . These applied torques are resisted by a torsional reaction at B. Determine the internal torque T as a function of x ...
Contents
Stresses in Beams | 198 |
Deflections of Beams | 265 |
Combined Stresses and Theories of Failure | 336 |
Column Theory and Analyses | 384 |
Statically Indeterminate Members | 432 |
Introduction to Component Design | 484 |
Analysis and Design for Inelastic Behavior | 523 |
Analysis and Design for Impact and Fatigue Loadings | 552 |
Selected Topics | 590 |
13 7 | 625 |
APPENDIX | 647 |
Index | 687 |
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Common terms and phrases
absolute maximum shear aluminum angle of twist applied Assume axes axial force axially loaded beam shown bending C₁ cantilever beam Castigliano's second theorem column compressive constant coordinate cross section cross-sectional area cylinder deflection deformation depicted in Fig diameter elastic curve equal equation equilibrium Euler EXAMPLE factor of safety FIGURE flexural stress FORTRAN free-body diagram k-ft k-in kN-m lb/ft length longitudinal M₁ material maximum shear stress modulus of elasticity Mohr's circle moment of inertia neutral axis normal stress obtained plane stress plane stress condition plot principal centroidal axis principal stresses r₁ radius ratio Refer to Fig rotation shaft shear force shear strain shown in Fig slope SOLUTION statically indeterminate steel stress element t₁ t₂ tensile Tmax torque torsional uniform load V₁ yield stress zero σ₁