## Introduction to Mechanics of Deformable Solids |

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Page 107

C . Now

replaced by a linear - viscoelastic bar of the simple Maxwell type , with E = 30 ,

000 , 000 psi , C = 20 , 000 psi per 0 . 002 percent strain in 10 , 000 hr at 80°F , a

= 7 X ...

C . Now

**consider**the aluminum bar as linear - elastic but the steel bar to bereplaced by a linear - viscoelastic bar of the simple Maxwell type , with E = 30 ,

000 , 000 psi , C = 20 , 000 psi per 0 . 002 percent strain in 10 , 000 hr at 80°F , a

= 7 X ...

Page 162

inside the other with no space between them ( Fig . 8 . 4 ) . How does this

assemblage differ from a hollow bar ( thick - walled cylinder ) under twist ? Recall

that ...

**Consider**a large number of concentric thin - walled circular cylinders nesting oneinside the other with no space between them ( Fig . 8 . 4 ) . How does this

assemblage differ from a hollow bar ( thick - walled cylinder ) under twist ? Recall

that ...

Page 236

the normal component of stress on on each plane . Select the plane on which

max , the maximum on , acts . If there is a choice , because more than one plane

is ...

**Consider**all planes through a given point at which stress is finite , and examinethe normal component of stress on on each plane . Select the plane on which

max , the maximum on , acts . If there is a choice , because more than one plane

is ...

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acting actual addition angle answer applied approximation assemblage axial force axis beam behavior bending circle circular column combined compatibility components compression compressive stress Consider constant creep cross section curve deflection deformation determined direction displacement effect elastic equal equation equations of equilibrium example Find force given gives homogeneous idealization increase initial interior isotropic length limit linear linear-elastic load material maximum Maxwell modulus moment nonlinear normal obtained plane plastic positive pressure principal Prob problem produced pure radius range ratio relation replaced requires response result rotation shear stress shell shown shows simple sketch solution solved statically steel strain stress-strain relations structural substitution Suppose surface symmetry temperature tensile tension tion tube twisting uniform virtual viscous yield zero