## Introduction to mechanics of deformable solids |

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Page 72

recoverable changes, an

decrease due to

the dead weights alone are not the actual stresses. A normal compressive stress

...

recoverable changes, an

**increase**in volume due to**increase**in tension and adecrease due to

**increase**in compression. Of course, the stresses computed fromthe dead weights alone are not the actual stresses. A normal compressive stress

...

Page 103

As R continues to

stress first at a value of R = RY. Figure 6.5 shows tube 2 reaching yield first (point

Y). Many design specifications limit the working load Ry, to some fraction of the

load ...

As R continues to

**increase**, one or the other of the tubes will reach the yieldstress first at a value of R = RY. Figure 6.5 shows tube 2 reaching yield first (point

Y). Many design specifications limit the working load Ry, to some fraction of the

load ...

Page 140

Pi = P2 = -fr0A P3 = +}a0A As the force in bar 4 cannot

further

magnitudes of the forces Pi, Pj, and P3. The algebraic sum of the forces must

remain zero.

Pi = P2 = -fr0A P3 = +}a0A As the force in bar 4 cannot

**increase**beyond oaA ,further

**increase**in moment M must be carried solely by**increases**in themagnitudes of the forces Pi, Pj, and P3. The algebraic sum of the forces must

remain zero.

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angle applied assemblage axial force beam behavior cantilever centroid circumferential column compatibility components of stress constant creep cross section cylinder dashpot deflection diameter direction displacement elastic-perfectly plastic elongation equation of virtual equations of equilibrium factor of safety free-body sketch homogeneous idealization increase inelastic initial interior pressure isotropic Kelvin Kelvin material limit linear Maxwell linear-elastic response linear-viscoelastic linear-viscous load maximum Maxwell material modulus Mohr's circle neutral axis nonlinear nonlinear-viscous normal stress outer perfectly plastic perpendicular plane plastic deformation plastic-limit principal stresses Prob problem pure bending radial radius ratio rotation shaft shear center shear strain shear stress shell shown in Fig simple shear solution statically statically determinate steel strain rate stress and strain stress-strain curve stress-strain relations Suppose surface symmetry temperature tensile stress thick-walled thickness time-dependent torsion twisting uniform unloading versus viscous yield curve yield stress zero