Introduction to Mechanics of Deformable Solids |
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Page 135
... SYMMETRY ABOUT BUT NOT IN THE PLANE OF BENDING The next step toward generality is to suppose that symmetry of the cross section about the y axis is preserved but that there is no symmetry about z . Consider- ing the assemblage as a ...
... SYMMETRY ABOUT BUT NOT IN THE PLANE OF BENDING The next step toward generality is to suppose that symmetry of the cross section about the y axis is preserved but that there is no symmetry about z . Consider- ing the assemblage as a ...
Page 136
... symmetric assemblage as in the unsymmetric ones corresponding to ( c ) and ( d ) . The response of a symmetric assemblage is no longer antisymmetric in pairs when the axis of rotation of the end plate is not an axis of symmetry of the ...
... symmetric assemblage as in the unsymmetric ones corresponding to ( c ) and ( d ) . The response of a symmetric assemblage is no longer antisymmetric in pairs when the axis of rotation of the end plate is not an axis of symmetry of the ...
Page 170
... symmetry of the cross section . These four axes of geometric symmetry , located in the cross section which lies halfway between the ends , cannot warp out of their plane or distort in their plane . Therefore , if uniformity along the ...
... symmetry of the cross section . These four axes of geometric symmetry , located in the cross section which lies halfway between the ends , cannot warp out of their plane or distort in their plane . Therefore , if uniformity along the ...
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Common terms and phrases
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