Introduction to Mechanics of Deformable Solids |
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Page 72
Of course , the stresses computed from the dead weights alone are not the actual
stresses . A normal compressive stress po must be added on every plane through
the material . As seen in Fig . 5 . 1 , the standard tension test then starts out as ...
Of course , the stresses computed from the dead weights alone are not the actual
stresses . A normal compressive stress po must be added on every plane through
the material . As seen in Fig . 5 . 1 , the standard tension test then starts out as ...
Page 233
16 Plane stress - zero cannot be ignored . 01 - 03 ( a ) Tmax = ' 1 = " > or ( 6 ) ...
Heavy dashed lines replace the heavy full lines of ( a ) to ( d ) to emphasize that
now the maximum compressive stress is sought . When either 0 ; or oy or both
are ...
16 Plane stress - zero cannot be ignored . 01 - 03 ( a ) Tmax = ' 1 = " > or ( 6 ) ...
Heavy dashed lines replace the heavy full lines of ( a ) to ( d ) to emphasize that
now the maximum compressive stress is sought . When either 0 ; or oy or both
are ...
Page 414
A small bending moment M is added to a bar element of length Ax , while the
axial compression P is maintained constant . At each point where the bending
action adds ( Aer | to the compressive strain ea , the normal compressive stress
on the ...
A small bending moment M is added to a bar element of length Ax , while the
axial compression P is maintained constant . At each point where the bending
action adds ( Aer | to the compressive strain ea , the normal compressive stress
on the ...
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Common terms and phrases
acts actual addition angle answer applied assemblage axial axis beam behavior bending carry circle circular column combined compatibility components compression compressive stress Consider constant creep cross section curve deflection deformation determined diameter dimensions direction displacement effect elastic equal equation example Figure Find force given gives homogeneous idealization increase independent 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 response result rotation shear stress shell shown shows simple sketch solution steel strain stress-strain relations structural Suppose surface symmetry temperature tensile tension thickness thin-walled tube twisting uniform unloading versus viscous yield zero
Bibliographic information
| Title | Introduction to Mechanics of Deformable Solids |
| Author | Daniel Charles Drucker |
| Publisher | McGraw-Hill, 1967 |
| Original from | the University of California |
| Digitized | 11 Mar 2008 |
| Length | 445 pages |
| Export Citation | BiBTeX EndNote RefMan |