## Introduction to Mechanics of Deformable Solids |

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Page 5

1 General Discussion of Stress 218 11 . 2 Principal Stresses in Two

Plane Stress ) 224 Principal values giren 224 Stress components Oz , Oy , Tay =

Tyr = 1 given 229 11 . 3 Problems of Two -

1 General Discussion of Stress 218 11 . 2 Principal Stresses in Two

**Dimensions**(Plane Stress ) 224 Principal values giren 224 Stress components Oz , Oy , Tay =

Tyr = 1 given 229 11 . 3 Problems of Two -

**dimensional**States of Stress 234 11 ...Page 259

20 Suppose that a linear - elastic bar of the

part of a rather complicated structure . The function of the three rosettes is to

determine the unknown magnitudes and signs of M , N , and T . All other

components ...

20 Suppose that a linear - elastic bar of the

**dimensions**given in Prob . 11 . 16 ispart of a rather complicated structure . The function of the three rosettes is to

determine the unknown magnitudes and signs of M , N , and T . All other

components ...

Page 440

8 Offset yield strength , 11 , 58 One -

Overhanging beam , 334 Path independence , 277 Perfectly plastic material , 16 ,

19 , 274 ( See also Plastic ) Permanent set or strain , 10 , 11 , 58 Photoelastic

coatings ...

8 Offset yield strength , 11 , 58 One -

**dimensional**problem , 185 , 331Overhanging beam , 334 Path independence , 277 Perfectly plastic material , 16 ,

19 , 274 ( See also Plastic ) Permanent set or strain , 10 , 11 , 58 Photoelastic

coatings ...

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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