Introduction to Mechanics of Deformable Solids |
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Page 94
A . Consider the force FA to be applied abruptly , to be held constant for a long
time , and then to be removed abruptly and to remain at zero . Describe clearly
and explicitly the motion of point A at each instant of time as a result of this
loading ...
A . Consider the force FA to be applied abruptly , to be held constant for a long
time , and then to be removed abruptly and to remain at zero . Describe clearly
and explicitly the motion of point A at each instant of time as a result of this
loading ...
Page 185
Development of a feeling for permissible idealizations and approximations is
possible only by comparison of the results obtained for more elementary
problems with the exact answers for these problems . A secondary reason for the
study of ...
Development of a feeling for permissible idealizations and approximations is
possible only by comparison of the results obtained for more elementary
problems with the exact answers for these problems . A secondary reason for the
study of ...
Page 230
The result , however , can be written down without going through the entire
process of summation of forces , etc . ... 2 : 10 , 11 ) , with oz in place of oa and Oy
in place of Oc . When a acts alone , the result is the last term , as derived in Sec .
4 .
The result , however , can be written down without going through the entire
process of summation of forces , etc . ... 2 : 10 , 11 ) , with oz in place of oa and Oy
in place of Oc . When a acts alone , the result is the last term , as derived in Sec .
4 .
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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