Introduction to Mechanics of Deformable Solids |
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Page 174
Compute and sketch the distribution of shear stress and shear strain over the
combined cross section of the inner and the outer cylinder : A . Immediately upon
application of T B . After a long time has elapsed 8 . 10 A 3 - in . - diameter 15 - in
.
Compute and sketch the distribution of shear stress and shear strain over the
combined cross section of the inner and the outer cylinder : A . Immediately upon
application of T B . After a long time has elapsed 8 . 10 A 3 - in . - diameter 15 - in
.
Page 224
11.7 Components of stress on an inclined plane in a biaxial stress field o a , Oc .
The two - dimensional sketch is adequate , but the true three - dimensional
situation must always be kept in mind . Zero values are significant numbers , not ...
11.7 Components of stress on an inclined plane in a biaxial stress field o a , Oc .
The two - dimensional sketch is adequate , but the true three - dimensional
situation must always be kept in mind . Zero values are significant numbers , not ...
Page 258
001 in . in diameter , and twisted through 0 . 5o . A . Find the principal strains in
the surface , and show their orientation on a sketch of the tube . B . Find the
normal strain en in the surface at + 30° and at - 30° to the circumferential
direction .
001 in . in diameter , and twisted through 0 . 5o . A . Find the principal strains in
the surface , and show their orientation on a sketch of the tube . B . Find the
normal strain en in the surface at + 30° and at - 30° to the circumferential
direction .
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actual addition angle answer applied assemblage axial axis beam behavior bending circle circular column combined components compression compressive stress computed Consider constant creep cross section curve cylinder deflection deformation determined diameter direction displacement effect elastic equal equation equilibrium 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 residual response result rotation shaft shear stress shell shown shows simple sketch solid solution steel strain stress-strain relations structural Suppose surface symmetry temperature tensile tension thickness thin-walled torsion tube twisting uniform unloading viscous yield zero