## Introduction to Mechanics of Deformable Solids |

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Page 61

1 Model

y = 7 / G dy = dret dyp O , E E , C , c . E = o / E de = des + dep dy Linear - viscous I

dt * c dy - 1 do Linear Maxwell 1 de 1 do 10 Linear Kelvin = Gx2 + come out o ...

1 Model

**Simple**shear Uniaxial tension All Linear - elastic Plastic 1 , 7 G , C . , Coy = 7 / G dy = dret dyp O , E E , C , c . E = o / E de = des + dep dy Linear - viscous I

dt * c dy - 1 do Linear Maxwell 1 de 1 do 10 Linear Kelvin = Gx2 + come out o ...

Page 65

The square distorts to a rhombus . The diagonals remain at right angles to each

other after the deformation so that in

these 45° directions , both of which rotate clockwise through the small angle r / 2 .

The square distorts to a rhombus . The diagonals remain at right angles to each

other after the deformation so that in

**simple**shear there is no shear strain forthese 45° directions , both of which rotate clockwise through the small angle r / 2 .

Page 276

Most of these and similar questions can be answered by starting over again from

well - established first principles and employing a minimum of mathematics .

Uniaxial tension or

elastic ...

Most of these and similar questions can be answered by starting over again from

well - established first principles and employing a minimum of mathematics .

Uniaxial tension or

**simple**shear The isothermal stress - strain relation of anelastic ...

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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