Introduction to Mechanics of Deformable Solids |
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Page 48
... components of stress or force per unit area will vary with the orientation of the plane of cut ( Figs . 1.1 , 1.4 ) . A rectangular prism of arbitrary size and position , with its axis parallel to the axis of the bar , is sketched ...
... components of stress or force per unit area will vary with the orientation of the plane of cut ( Figs . 1.1 , 1.4 ) . A rectangular prism of arbitrary size and position , with its axis parallel to the axis of the bar , is sketched ...
Page 237
... components remaining are labeled with a question mark . They are equivalent to those labeled Tz = T1 and T2 = Tan in Fig . 11.176 . Now it is obvious that each of these shear components must be zero . If not , the view of the ...
... components remaining are labeled with a question mark . They are equivalent to those labeled Tz = T1 and T2 = Tan in Fig . 11.176 . Now it is obvious that each of these shear components must be zero . If not , the view of the ...
Page 269
... components of strain and the components of stress , to represent time rate of change , converts all the stress - strain relations ( 12.2 : 2-16 ) to appropriate forms for the rates . In particular , then , Eqs . ( 12.2 : 13 , 14 ) with ...
... components of strain and the components of stress , to represent time rate of change , converts all the stress - strain relations ( 12.2 : 2-16 ) to appropriate forms for the rates . In particular , then , Eqs . ( 12.2 : 13 , 14 ) with ...
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actual addition angle answer applied assemblage axes axial axis beam behavior bending circle circular column 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 replaced requires 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