Introduction to Mechanics of Deformable Solids |
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Page 314
... gives 2 / L from the first equality in Eq . ( 13.5 : 4 ) . In turn , these ratios give del / oal , Oc2 / 0a2 , which determine σe / ae2 , then p / pa , and finally R / pαπα ?. έα = Thick - walled cylinder , p = 0 , plane strain The ...
... gives 2 / L from the first equality in Eq . ( 13.5 : 4 ) . In turn , these ratios give del / oal , Oc2 / 0a2 , which determine σe / ae2 , then p / pa , and finally R / pαπα ?. έα = Thick - walled cylinder , p = 0 , plane strain The ...
Page 382
... gives 811 ( a + b + c ) = 810C +812 ( a + b ) after a little rearranging and multiplication by a + b + c . ( 15.2 : 2 ) Equation ( 15.2 : 2 ) is the geometric constraint imposed by the rigid bar for any loading ( see Sec . 6.4 ) ...
... gives 811 ( a + b + c ) = 810C +812 ( a + b ) after a little rearranging and multiplication by a + b + c . ( 15.2 : 2 ) Equation ( 15.2 : 2 ) is the geometric constraint imposed by the rigid bar for any loading ( see Sec . 6.4 ) ...
Page 399
... gives the actual limit load , and Fig . 15.9a is the correct collapse configuration . Although ( 15.5 : 10 ) gives a better answer than ( 15.5 : 9 ) when M " < 17M , it is not the best answer . The plastic hinge for positive moment ...
... gives the actual limit load , and Fig . 15.9a is the correct collapse configuration . Although ( 15.5 : 10 ) gives a better answer than ( 15.5 : 9 ) when M " < 17M , it is not the best answer . The plastic hinge for positive moment ...
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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