## Introduction to Mechanics of Deformable Solids |

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Page 340

point of maximum

the maximum ( really minimum ) point Xm . If the 0 < x < a set is used , 0 = Radm

? + c or ? m ? = - 21 = L to - 5 ( 1 - ) " - TO ( 14 . 4 : 13 ) This answer is valid only ...

point of maximum

**deflection**and for lvmax itself . The slope of the beam is zero atthe maximum ( really minimum ) point Xm . If the 0 < x < a set is used , 0 = Radm

? + c or ? m ? = - 21 = L to - 5 ( 1 - ) " - TO ( 14 . 4 : 13 ) This answer is valid only ...

Page 368

When the material is nonlinear , the orientation and the position of the neutral

axis usually will alter from one cross section to the next ; the direction of the

is ...

When the material is nonlinear , the orientation and the position of the neutral

axis usually will alter from one cross section to the next ; the direction of the

**deflection**and the pattern of stress and strain distribution will change as the loadis ...

Page 403

RR = F # MB = FH < FL M N Large

theory 0 . 5 Fig . 16 . 1 Large

material . From K . E . Bisshopp and D . C . Drucker , Large

Cantilever ...

RR = F # MB = FH < FL M N Large

**deflection**theory FL2 / 3E1 Small**deflection**theory 0 . 5 Fig . 16 . 1 Large

**deflection**of beams . ( c ) Beam of linear - elasticmaterial . From K . E . Bisshopp and D . C . Drucker , Large

**Deflection**ofCantilever ...

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acting actual addition angle answer applied approximation assemblage axial force axis beam behavior bending circle circular column combined compatibility components compression compressive stress Consider constant creep cross section curve deflection deformation determined direction displacement effect elastic equal equation equations of equilibrium example Find force given gives homogeneous idealization increase initial interior isotropic length limit linear linear-elastic load material maximum Maxwell modulus moment nonlinear normal obtained 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 solved statically steel strain stress-strain relations structural substitution Suppose surface symmetry temperature tensile tension tion tube twisting uniform virtual viscous yield zero