## Engineering mechanics of materials |

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Page 452

The length / of the

2. Other needed dimensions are shown in Figure 9.5(a). Assume the coefficient

of thermal expansion for

The length / of the

**aluminum**rods is 20 in. and their cross-sectional area A is 1 in.2. Other needed dimensions are shown in Figure 9.5(a). Assume the coefficient

of thermal expansion for

**aluminum**, a = 12.5 x 106 in./in./°F, the modulus of ...Page 630

13.24 An

and subjected to an impact loading by dropping a weight W from a height h onto

the midpoint of each beam. The length of the

...

13.24 An

**aluminum**beam and a steel beam are simply supported at their endsand subjected to an impact loading by dropping a weight W from a height h onto

the midpoint of each beam. The length of the

**aluminum**beam is 0.30 m and each...

Page 685

A concentrated load P = 5000 lb is placed at the free end acting in a plane that

contains the v principal axis of inertia. Let Eti = 10 x 106 psi and £br = 15 x 106

psi and deter- FIGURE H14.26 mine the maximum flexural stresses in the

A concentrated load P = 5000 lb is placed at the free end acting in a plane that

contains the v principal axis of inertia. Let Eti = 10 x 106 psi and £br = 15 x 106

psi and deter- FIGURE H14.26 mine the maximum flexural stresses in the

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### Contents

Internal Forces in Members | 1 |

Hollow Circular ShaftsAngle of Twist and Shearing Stresses | 157 |

4i5 Power Transmission | 169 |

Copyright | |

7 other sections not shown

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### Common terms and phrases

absolute maximum shear allowable stress aluminum angle of twist applied Assume axial force axially loaded beam shown bending cantilever beam Castigliano's second theorem circular column components compressive Compute constant construct coordinate cross section cross-sectional area cylinder deflection deformation depicted in Figure Determine diameter differential elastic curve equal equation equilibrium factor of safety flexural stress free-body diagram function given by Eq Homework Problems k-ft k-in kN-m length longitudinal material maximum shear stress modulus of elasticity Mohr's circle neutral axis normal stress obtained perpendicular plane stress plot principal centroidal axis principal stresses radius Refer to Figure respect rotation section a-a segment shear center shear force shear strain shown in Figure slope Solution Solve static statically indeterminate steel stress element subjected Substitution tension tion torque torsional uniform load vertical yield strength yield stress zero