## Introduction to Mechanics of Deformable Solids |

### From inside the book

Results 1-3 of 70

Page 154

A . When the extreme fiber stress ( the

moments 1 . M , Y 2 . M , ' 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 o , find themoments 1 . M , Y 2 . M , ' about the coordinate axes . B . When the beam is

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

neutral ...

Page 220

T max T max Fig . 11 . 2 Planes of

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

greatest , and on another algebraically the least , normal stress for any plane

through the ...

T max T max Fig . 11 . 2 Planes of

**maximum**shear stress ( see Fig . 11 . 1 ) . 01Tmax = v angle BAC = angle ABC = 45° 2 braically ( tension positive ) the

greatest , and on another algebraically the least , normal stress for any plane

through the ...

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 .

### What people are saying - Write a review

We haven't found any reviews in the usual places.

### Other editions - View all

### Common terms and phrases

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 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 viscous yield zero