Elasticity

Domain

Remarks

Hooke's Law

  • Change in shape & size of a body is proportional to the change in applied loads
  • Within the range of "elastic region"
  • Clearly illustrated in stress-strain curves

Elastic region

  • No permanent deformation suffered
  • Linearly elastic: deformed strain directly proportional to applied stress & plot is straight line
  • Gradient = Young's modulus, E constant
  • Non-linearly elastic: deformed strain unproportional to stress
  • E(e ) is function of strain, varies
  • Note:
  • Both linearly & non-linearly elastic deformation follows their respective stress-strain paths during loading & unloading
  • Typical of lightly-loaded homogeneous, isotropic materials

Non-elastic region

  • Loading stress-strain path is different from unloading stress-strain path
  • Temporary & permanent deformations
  • E varies w.r.t. strain & stress path, orientation, rate, etc. à tangent modulus E(s , n , e )
  • Hysteresis, phase transition, irregularities, imperfections & other phenomena account for the difference
  • Typical of anisotropic, multi-phased materials like soil & polymers

Properties often required for analysis

  • E: Young's modulus; within l-elastic region, is ratio of axial stress / axial strain
  • n : Poisson's ratio; -ve ratio of lateral strain / longitudinal strain; [0,0.5] à brittle/rigid material: low n à ductile material: high n
  • G: shear modulus of elasticity; G=E/2.(1+n ); ratio of shear stress / shear strain
  • K: bulk modulus of elasticity; K=E/3.(1-2.n ); ratio of mean normal stress / dilatation (volumetric strain)

Brittle / rigid materials

  • Low n
  • High E, G
  • Low K
  • Low ultimate strain

Ductile materials

  • High n
  • Low E, G
  • High K
  • High ultimate strain

Stress-strain

  • Normal direction: Poisson effect
  • e = f(s , E, n )
  • Shear direction: no Poisson effect
  • g = f(t , G)

Implications on normal stress-strain

  • Normal strain can be induced, under zero stress in that direction
  • Due to Poisson's ratio
  • Normal stresses & strains cause change in size & volume
  • No failure: equal triaxial normal stresses
  • In linearly-elastic region, g xy = 2.e

Implications on shear stress-strain

  • Shear strain is only influenced by shear stress; no Poisson's ratio
  • Only shear strain is induced by shear stress in that direction
  • Shear stresses & strains cause change in shape (distortion) only
  • Failure: under unequal triaxial normal stresses, causing shear distortion

Elasticity relation

  • {s } = {D} . {e }
  • Poisson effect: stress & strain are coupled

State of stress-strain

  • State of stress: complete description of stresses at a point à using consistent coordinate system: Cartesian, polar, cylindrical
  • Plane stress: no out-of-plane stress; e.g. on free surface
  • State of strain: complete description of strains at a point
  • Plane strain: no out-of-plane strain; e.g. planes across straight, long, prismatic, homogeneous structures
  • Axisymmetric: stress & strain invariant with angle of revolution of a pressure cylinder
  • Poisson effect: normal in-plane & out-of-plane strains coupled à plane stress cannot occur simultaneously with plane strain

Stress transformation

  • Equilibrium
  • State of stress at a point varies with {loads, locations, time, orientation planes}
  • Principal stress: max. stress at point orientation
  • Principal normal stress p.n.s.: zero shear stress
  • Principal shear stress: 45° to p.n.s.; av. n.s.
  • Retrofit or reinforce along principal stress directions
  • Mohr’s circle

Strain transformation

  • Compatibility
  • State of strain at a point varies with {geometry, locations, time, orientation planes}
  • Principal strain: max. stress at point orientation
  • Principal normal strain p.n.s.: zero shear strain
  • Principal shear strain: 45° to p.n.s.; av. n.s.
  • Restrain along principal strain directions
  • Mohr’s circle

3-D absolute max shear

  • Occurs in-plane: if principal stresses or strains are opposite à tension-compression or compression-tension
  • Occurs out-of-plane: if principal stresses or strains are same à tension-tension or compression-compression

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