## Introduction to Mechanics of Deformable Solids |

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Page 220

Tmax = _ 01 - 03 T max = 2 angle BAC = angle ABC = 45° braically ( tension

positive ) the greatest , and on another algebraically the least ,

any plane through the point . Call the maximum principal stress o 1 and the

minimum ...

Tmax = _ 01 - 03 T max = 2 angle BAC = angle ABC = 45° braically ( tension

positive ) the greatest , and on another algebraically the least ,

**normal**stress forany plane through the point . Call the maximum principal stress o 1 and the

minimum ...

Page 229

Intersection with the circle at the point ( ov , tyz ) gives the

components of stress acting on the plane . In this illustrative example , the

stress is negative , or compressive , whereas the shear stress is positive , or ...

Intersection with the circle at the point ( ov , tyz ) gives the

**normal**and shearcomponents of stress acting on the plane . In this illustrative example , the

**normal**stress is negative , or compressive , whereas the shear stress is positive , or ...

Page 237

However , max is the greatest

component 7 must be zero . Similarly , consideration of the picture observed in

the direction of oß , with stress components Omax , 0q , ? , shows the second

component ...

However , max is the greatest

**normal**stress for any plane . Therefore thiscomponent 7 must be zero . Similarly , consideration of the picture observed in

the direction of oß , with stress components Omax , 0q , ? , shows the second

component ...

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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