## Introduction to Mechanics of Deformable Solids |

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Page 154

A . When the extreme fiber stress ( the

moments 1 . MY 2 . M , Y about the coordinate axes . B . When the beam is

essentially fully plastic ( oo everywhere except the immediate vicinity of the

neutral ...

A . When the extreme fiber stress ( the

**maximum**stress ) just reaches oo , find themoments 1 . MY 2 . M , Y about the coordinate axes . B . When the beam is

essentially fully plastic ( oo everywhere except the immediate vicinity of the

neutral ...

Page 220

2 Planes of

angle BAC = angle ABC = 45° braically ( tension positive ) the greatest , and on

another algebraically the least , normal stress for any plane through the point .

2 Planes of

**maximum**shear stress ( see Fig . 11 . 1 ) . Tmax = _ 01 - 03 T max = 2angle BAC = angle ABC = 45° braically ( tension positive ) the greatest , and on

another algebraically the least , normal stress for any plane through the point .

Page 375

B . Compute the algebraic

Indicate where each acts on a sketch of the frame . C . If you solved Prob . 1 . 1

previously , evaluate the answer you gave then . 14 . 36 Parts of Prob . 14 .

B . Compute the algebraic

**maximum**of oz and the numeric**maximum**at A - A .Indicate where each acts on a sketch of the frame . C . If you solved Prob . 1 . 1

previously , evaluate the answer you gave then . 14 . 36 Parts of Prob . 14 .

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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