Introduction to Mechanics of Deformable Solids |
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Page 171
... twisting must remain a right angle after twisting ( Fig . 8.116 ) . The warping of each and every cross section which results is as shown in Fig . 8.11a for the reference cross section of zero rotation which lies halfway between the ...
... twisting must remain a right angle after twisting ( Fig . 8.116 ) . The warping of each and every cross section which results is as shown in Fig . 8.11a for the reference cross section of zero rotation which lies halfway between the ...
Page 174
... twisting moment T is applied abruptly to the assemblage . Compute and sketch the distribution of shear stress and shear strain over the combined cross section of the inner and the outer cylinder : A. Immediately upon application of T B ...
... twisting moment T is applied abruptly to the assemblage . Compute and sketch the distribution of shear stress and shear strain over the combined cross section of the inner and the outer cylinder : A. Immediately upon application of T B ...
Page 235
... twisting moment of 300,000 in./lb . The method of solution must start from first principles with a free - body sketch . Consider the effects of rotation , pressure , and twisting moment , and show and explain all steps . B. Find the ...
... twisting moment of 300,000 in./lb . The method of solution must start from first principles with a free - body sketch . Consider the effects of rotation , pressure , and twisting moment , and show and explain all steps . B. Find 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