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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aluminum applied assemblage axial force beam behavior change in length circle circumferential column components of stress computed constant cross section cylinder dashpot deflection diameter dimensions direction displacement elastic elastic-perfectly plastic elongation equations of equilibrium factor of safety free-body sketch homogeneous HR steel idealization increase inelastic initial interior pressure isotropic Kelvin material linear Maxwell linear-elastic linear-viscous load M₂ maximum Maxwell material modulus Mohr's circle neutral axis nonlinear normal stress outer P₁ P₂ perfectly plastic perpendicular plane plastic deformation plastic-limit Prob problem pure bending radial radius ratio residual stress rotation shaft shear strain shear stress shell shown in Fig simple shear simple tension solution statically statically indeterminate stress and strain stress-strain curve stress-strain relations structural Suppose surface symmetry t₁ temperature tensile stress thick-walled thickness time-dependent torsion uniaxial uniform unloading versus viscous yield point yield stress Young's modulus zero ΕΙ σα σο στ