Introduction to Mechanics of Deformable Solids |
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Page 202
Suppose that a particular set of values é ' , de ' / dt , o ' , do ' / dt , M ' , dM ' / dt , . . .
satisfies equilibrium , compatibility , and the stress - strain relations everywhere
for one loading of a body and that another solution for the same body under a ...
Suppose that a particular set of values é ' , de ' / dt , o ' , do ' / dt , M ' , dM ' / dt , . . .
satisfies equilibrium , compatibility , and the stress - strain relations everywhere
for one loading of a body and that another solution for the same body under a ...
Page 377
Of course , unless at least some of the salient features of the actual , or real , state
( which satisfies both equilibrium and compatibility ) appear either in the
equilibrium set or in the compatible set , no information about the real problem
will be ...
Of course , unless at least some of the salient features of the actual , or real , state
( which satisfies both equilibrium and compatibility ) appear either in the
equilibrium set or in the compatible set , no information about the real problem
will be ...
Page 381
If the equilibrium set Fi , M ' is chosen to be the actual set F , M , FA * = * * | M dx
where At , the downward deflection under the load , is – v * at x = a , * A1 = 4věta
40 ) and M = Rax for 0 < x < a , M = RAX – F ( x – a ) for a < x < a + b . Fate Fat = L
...
If the equilibrium set Fi , M ' is chosen to be the actual set F , M , FA * = * * | M dx
where At , the downward deflection under the load , is – v * at x = a , * A1 = 4věta
40 ) and M = Rax for 0 < x < a , M = RAX – F ( x – a ) for a < x < a + b . Fate Fat = L
...
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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