## Engineering mechanics of materialsThis book provides the students of various engineering disciplines with a clear and understandable treatment of the concepts of Mechanics of Materials or Strength of Materials. This subject is concerned with the behavior of deformable bodies when subjected to axial, torsional and flexural loads as well as combinations thereof. It is a 3rd, updated edition of the popular undergraduate level textbook useful for students of mechanical, structural, civil, aeronautical and other engineering disciplines. The book is supplied with problems and a solution manual will be available from the authors. |

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Page 315

A i Xjj + A2xl2 + /43Xj3 I Pa (2 \ I Pa (5 \ Pa The center

constant bending stiffness EIt of total length 4a subjected to a center loading P

equals |{Pa3/£/1). The ratio of these

of ...

A i Xjj + A2xl2 + /43Xj3 I Pa (2 \ I Pa (5 \ Pa The center

**deflection**of a beam withconstant bending stiffness EIt of total length 4a subjected to a center loading P

equals |{Pa3/£/1). The ratio of these

**deflections**is ff, which means that the beamof ...

Page 333

EXAMPLE C6.1 Write a FORTRAN program to determine the maximum rotation

and the

as shown in Fig. C6.1. Divide the span L into 10 parts and compute the

...

EXAMPLE C6.1 Write a FORTRAN program to determine the maximum rotation

and the

**deflections**of a cantilever beam with a loading that varies parabolicallyas shown in Fig. C6.1. Divide the span L into 10 parts and compute the

**deflection**...

Page 334

Write a FORTRAN program to determine the

beam which is loaded with a linearly varying loading as shown in Fig. C6.2.

Divide the span L into 10 parts and compute the

the ...

Write a FORTRAN program to determine the

**deflections**of a simply supportedbeam which is loaded with a linearly varying loading as shown in Fig. C6.2.

Divide the span L into 10 parts and compute the

**deflection**at these points alongthe ...

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### Contents

Stress Strain and Their Relationships | 60 |

Stresses and Strains in Axially Loaded Members | 121 |

Torsional Stresses Strains and Rotations | 159 |

Copyright | |

14 other sections not shown

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### Common terms and phrases

absolute maximum shear aluminum angle of twist applied Assume axial force axially loaded beam shown bending cantilever beam Castigliano's second theorem column compressive constant coordinate cross section cross-sectional area cylinder deflection deformation depicted in Fig elastic curve equal equation equilibrium Euler EXAMPLE factor of safety FIGURE flexural stress FORTRAN free-body diagram function given by Eq k-ft k-in kN-m lb/ft length longitudinal material maximum in-plane shear maximum shear stress modulus of elasticity Mohr's circle neutral axis normal stress obtained perpendicular plane stress condition plot positive principal centroidal axis principal strains principal stresses radius ratio reactions Refer to Fig respect rotation shear force shear strain shown in Fig simply supported beam slope SOLUTION Solve Problem statically indeterminate steel stress concentration stress element subjected torque torsional uniform load vertical yield strength yield stress zero