Introduction to Mechanics of Deformable Solids |
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Page 152
Fig . 7 . 30 Beam simulation by assemblage . All bars of the 13 - bar assemblage
are 1 in . ? except for the corner bars , which are 4 in . ( Actual beam A = 11 in . 2
) 7 . 8 / PROBLEMS OF ACTUAL BEAMS IN PURE BENDING OR ENFORCED ...
Fig . 7 . 30 Beam simulation by assemblage . All bars of the 13 - bar assemblage
are 1 in . ? except for the corner bars , which are 4 in . ( Actual beam A = 11 in . 2
) 7 . 8 / PROBLEMS OF ACTUAL BEAMS IN PURE BENDING OR ENFORCED ...
Page 154
The material of the beam is elastic - perfectly plastic , with yield stress 00 . A .
When the extreme fiber stress ( the maximum stress ) just reaches oo , find the
moments 1 . M , Y 2 . M , about the coordinate axes . B . When the beam is
essentially ...
The material of the beam is elastic - perfectly plastic , with yield stress 00 . A .
When the extreme fiber stress ( the maximum stress ) just reaches oo , find the
moments 1 . M , Y 2 . M , about the coordinate axes . B . When the beam is
essentially ...
Page 434
Beam , as one - dimensional continuum , 331 overhanging , 334 at plastic limit
load , 348 – 352 propped cantilever , 342 sandwich , 356 simply supported , 331
slope , 332 statically determinate , 334 , 338 - 341 statically indeterminate , 334 ...
Beam , as one - dimensional continuum , 331 overhanging , 334 at plastic limit
load , 348 – 352 propped cantilever , 342 sandwich , 356 simply supported , 331
slope , 332 statically determinate , 334 , 338 - 341 statically indeterminate , 334 ...
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actual addition angle answer applied assemblage axes axial axis beam behavior bending circle circular column combined 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 relation replaced requires residual 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 versus viscous yield zero