## Introduction to Mechanics of Deformable Solids |

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Page 220

01 Tmax = v angle BAC = angle ABC = 45° 2 braically ( tension positive ) the

greatest , and on another algebraically the least ,

through the point . Call the maximum principal stress 01 and the minimum

principal ...

01 Tmax = v angle BAC = angle ABC = 45° 2 braically ( tension positive ) the

greatest , and on another algebraically the least ,

**normal**stress for any planethrough the point . Call the maximum principal stress 01 and the minimum

principal ...

Page 229

11 . 12 drawn through the pole as shown in ( c ) . Intersection with the circle at the

point ( Oy , Tyr ) gives the

plane . In this illustrative example , the

...

11 . 12 drawn through the pole as shown in ( c ) . Intersection with the circle at the

point ( Oy , Tyr ) gives the

**normal**and shear components of stress acting on theplane . In this illustrative example , the

**normal**stress is negative , or compressive...

Page 237

However , Omax is the greatest

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

direction of ox , with stress components omax , on , ? , shows the second

component ...

However , Omax is the greatest

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

direction of ox , with stress components omax , on , ? , shows the second

component ...

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acts actual addition angle answer applied assemblage axial axis beam behavior bending carry circle circular column combined compatibility components compression compressive stress Consider constant creep cross section curve deflection deformation determined diameter dimensions direction displacement effect elastic equal equation example Figure Find force given gives homogeneous idealization increase independent 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 response result rotation shear stress shell shown shows simple sketch solution steel strain stress-strain relations structural Suppose surface symmetry temperature tensile tension thickness thin-walled tube twisting uniform unloading versus viscous yield zero