Introduction to Mechanics of Deformable Solids |
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Page 77
Linear - elastic response accompanying the biaxial stress o in the shell can be
found by adding the effect of the stresses at right angles to the effect of the stress
in any given direction . The circumferential elastic Ос da 0 tw oc oc we LFig .
Linear - elastic response accompanying the biaxial stress o in the shell can be
found by adding the effect of the stresses at right angles to the effect of the stress
in any given direction . The circumferential elastic Ос da 0 tw oc oc we LFig .
Page 109
What is the effect of temperature change and support movement on the plastic -
limit load ? B . Now replace bar 2 with a linear - viscous bar , and suppose that Fc
is increased abruptly from zero to 20 , 000 lb and then held constant . 1 .
What is the effect of temperature change and support movement on the plastic -
limit load ? B . Now replace bar 2 with a linear - viscous bar , and suppose that Fc
is increased abruptly from zero to 20 , 000 lb and then held constant . 1 .
Page 146
As the same material at different temperatures has quite different properties , the
net effect is equivalent to the combination of quite dissimilar materials at the
same temperature . If the beam is inhomogeneous , but of uniform cross section ...
As the same material at different temperatures has quite different properties , the
net effect is equivalent to the combination of quite dissimilar materials at the
same temperature . If the beam is inhomogeneous , but of uniform cross section ...
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actual addition angle answer applied assemblage axes axial axis beam behavior bending circle circular column combined compatibility components compression compressive stress 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 versus viscous yield zero