## Introduction to Mechanics of Deformable Solids |

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Page 247

11.23

respectively . Point A , originally on the x axis a distance Ax from 0 , goes to A ' .

11.23

**Displacement**, deformation , and distortion . torted in general . The**displacement**components of O are labeled u , v , w in the x , y , z directions ,respectively . Point A , originally on the x axis a distance Ax from 0 , goes to A ' .

Page 379

15.2 Part ( b ) shows discontinuous

logical choice for the arbitrary

Each bar ...

15.2 Part ( b ) shows discontinuous

**displacement**. Because of symmetry , alogical choice for the arbitrary

**displacement**field and compatible strains is to**displace**C down by A * , with the support points A and B remaining in position .Each bar ...

Page 390

Which layout is better ? Why ? What modification would you employ if the total

balance weight is restricted to 10 lb ? 15 . 2 Find vc , the downward vertical

component of

work . 15 .

Which layout is better ? Why ? What modification would you employ if the total

balance weight is restricted to 10 lb ? 15 . 2 Find vc , the downward vertical

component of

**displacement**of pin C ( Fig . 15 . 5 ) . Use the equation of virtualwork . 15 .

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