Introduction to Mechanics of Deformable Solids |
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Page 126
... actual stress and strain are used . This repetition is avoided by the use of the generalized forms . Nevertheless , it is the actual stress form which turns out most convenient for the elastic response to the bending of an assemblage of ...
... actual stress and strain are used . This repetition is avoided by the use of the generalized forms . Nevertheless , it is the actual stress form which turns out most convenient for the elastic response to the bending of an assemblage of ...
Page 152
... ( Actual beam A 11 in.2 ) = 7.8 / PROBLEMS OF ACTUAL BEAMS IN PURE BENDING OR ENFORCED ROTATION 7.20 Consider a beam of uniform cross section which is symmetric about the xy plane but not the xz plane . A pure bending moment M is applied ...
... ( Actual beam A 11 in.2 ) = 7.8 / PROBLEMS OF ACTUAL BEAMS IN PURE BENDING OR ENFORCED ROTATION 7.20 Consider a beam of uniform cross section which is symmetric about the xy plane but not the xz plane . A pure bending moment M is applied ...
Page 389
... actual problem . When the displacements and strains of the actual system are considered , 8 , for example , may depend upon N , My , M2 , and T in combination . Linear - elastic systems are decoupled to the extent that each component of ...
... actual problem . When the displacements and strains of the actual system are considered , 8 , for example , may depend upon N , My , M2 , and T in combination . Linear - elastic systems are decoupled to the extent that each component of ...
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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