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Lecture 3 mohr’s circle and theory of failure
Unit 1- Stress and Strain
Topics Covered
  Lecture -1 - Introduction, state of plane stress

  Lecture -2 - Principle Stresses and Strains

  Lecture -3 - Mohr's Stress Circle and Theory of
   Failure

  Lecture -4- 3-D stress and strain, Equilibrium
   equations and impact loading

  Lecture -5 - Generalized Hook's law and Castigliono's
Mohr Stress Circle
         We derived these two equations- These equations represent the equation of
         a circle
                      σ1 + σ2 σ1 − σ2
                 σn =         +        cos2θ + τ sin2θ
                         2         2
                          σ1 − σ2
                    σt =          sin2θ − τ cos2θ
                             2
    €    ⎛     σ1 + σ2 ⎞ 2 ⎛ σ1 − σ2                 ⎞ 2
         ⎜σn −         ⎟ = ⎜         cos2θ + τ sin2θ ⎟
        €
         ⎝        2 ⎠ ⎝ 2                            ⎠
                        2     ⎛ σ1 − σ2                 ⎞ 2
                (σt )       = ⎜
                              ⎝ 2
                                         sin2θ − τ cos2θ ⎟
                                                         ⎠

€
Mohr Stress Circle
            ⎛     σ1 + σ2 ⎞ 2 ⎛ σ1 − σ2                 ⎞ 2
            ⎜σn −         ⎟ = ⎜         cos2θ + τ sin2θ ⎟
            ⎝        2 ⎠ ⎝ 2                            ⎠
                          2     ⎛ σ1 − σ2                 ⎞ 2
                  (σt )       = ⎜
                                ⎝ 2
                                           sin2θ − τ cos2θ ⎟
                                                           ⎠
                   Add above 2 equations. We will equation of circle.
€                                 2                          2
               ⎛    σ + σ ⎞
                         1      2
                                    ⎛ σ − σ ⎞
                                          2        1   2  2
               ⎜σ −
                  n        ⎟ + σ = ⎜    t  ⎟ + (τ )
        €      ⎝      2 ⎠         ⎝ 2 ⎠

                               2           2
                 ( x − a)              y                       r   2
                                                                        Equation of circle

    €
Mohr Stress Circle
  Graphical method to determine stresses.
     Body subjected to two mutually perpendicular principal
      stresses of unequal magnitude.
     Body subjected to two mutually perpendicular principal
      stresses of unequal magnitude and unlike (one tensile
      and other compressive).
     Body subjected to two mutually perpendicular principal
      stresses + simple shear stress.
Mohr Stress Circle
      Body subjected to two mutually perpendicular
         principal stresses of unequal magnitude
                      (σ1 - σ2 )                 length AD = Normal stress on oblique plane
            σt
                                                             = σn
                                     E           length ED = Tangential stress on Oblique plane
                                                             = σt
                                    2θ 	

   B length AE = Resultant stress on Oblique plane
                        θ 	

                   σn
                                O   D        σ1                     2         2
A                C                                          = σ +σt         n
                                             €
    σ2
                 σ1                          €
                                         €
Mohr Stress Circle
           Body subjected to two mutually perpendicular principal
            stresses of unequal magnitude and unlike (one tensile
            and other compressive).
               (σ1+σ2 )
                                                  length AD = Normal stress on oblique plane
    σt                               E                        = σn
                                                  length ED = Tangential stress on Oblique plane
                                                              = σt
                                2θ 	

             length AE = Resultant stress on Oblique plane
C              θ 	

                     B
                                             σn                        2        2
           A           O           D                         = σt + σn
_
                                             €
               +           σ1
     σ2
                                             €
                                             €
Mohr Stress Circle
           Body subjected to two mutually perpendicular principal
            stresses + simple shear stress.

            σt                           length AD = Normal stress on oblique plane
                                                     = σn
                                 E       length ED = Tangential stress on Oblique plane

                            2θ 	

                                                     = σt
                                     length AE = Resultant stress on Oblique plane
                                 B M σ
                                       n
                  L C           D σ1                      2         2
A                       O                           = σ +σ
                                                        t         n
                                     €
    σ2
                 σ1                  €
                                     €
Theories of failure
  Maximum principal stress (Rankine theory)

  Maximum principal strain (Saint Venant theory)

  Maximum shear stress (Guest theory)

  Maximum strain energy (Haigh theory)

  Maximum shear strain energy (Mises & Henky
   theory)
1. Maximum principal
                    stress theory
           σ1,σ2 ,σ3 =principal stresses in 3 perpendicular
                                directions

                                                               *
                              max(σ1,σ2 ,σ3 ) ≤ σ
€
    Maximum principal stress should be less than the max stress (yield stress) that material
    can bear in tension or compression.
            *
         σ = max tensile or compressive strength of material
          €
                                                                           σ*
                                             max principal stress=
                                                                     safety _ factor
2. Maximum principal
                        strain theory
               σ1,σ2 ,σ3 =principal stresses in 3 perpendicular
                                     directions
                   σ1 υσ2 υσ3                 σ2 υσ1 υσ3                    σ3 υσ1 υσ2
               e1 = −    −                e2 = −    −                   e3 = −    −
                   E E     E                  E E     E                     E E     E
                                                                  *              σ*
€                                  max(e1,e2 ,e3 ) ≤ e                        *
                                                                             e =
                                                                                 E
                *
            σ       = max tensile or compressive strength of material
    € Maximum principal strain should be less than the max strain (yield strain) that material
                          €                          €
      can bear in tension or compression.                        €
                                                                                σ*
              €                                   max principal stress=
                                                                          safety _ factor
3. Maximum shear stress
               theory
   max shear stress =half the difference of max and min principal stresses
                      1
                     = (σ1 − σ3 )
                      2                                          In simple tension the stress
To prevent failure max shear stress should be less that shear    is existing in one direction
stress in simple tension at elastic limit
                                        1 *        *
                                       = (σt − 0) σt
             max shear stress at elastic limit                        = max tensile of material
     €                                  2
                          (σ1 − σ 3 ) ≤ σ *
                                          t
Maximum shear stress should be less than the max shear stress in simple tension (at
elastic limit) that material can bear.
                                   €             €
                                                                             σ*t
                                                 allowable stress =
    €                                                                  safety _ factor
4. Maximum strain
                         energy theory
    Strain energy per unit volume should be less than the strain energy per unit volume in
    simple tension (at elastic limit) that material can bear.


                                                                                    2
               [σ 2
                  1   + σ + σ − 2υ (σ1σ2 + σ1σ3 + σ2σ3 ) ≤ (σ
                         2
                         2
                                2
                                3                                   ]       *
                                                                            t   )
                                                    σ*t
                      max allowable stress=
                                              safety _ factor
€


                               €
5. Maximum shear strain
            energy theory
Shear strain energy per unit volume should be less than the shear strain energy per unit
volume in simple tension (at elastic limit).


                         2                2                2                      2
            (σ1 − σ2 ) + (σ1 − σ3 ) + (σ2 − σ3 )               ≤ 2 * (σ   *
                                                                          t   )
                                                σ*t
                  max allowable stress=
                                          safety _ factor
€


                             €
Important points
  Brittle material -> Max principal stress
     Brittle material do not fail in shear

  Ductile material -> Max shear stress/max shear strain
   energy
     Ductile material fail in shear because their yield
       strength is high.
Failure Theory
  PROBLEM- The principal stresses at a point in an
   elastic material are 200 N/mm2 (tensile), 100 N/
   mm2 (tensile) and 50 N/mm2 (compressive). If the
   stresses at the elastic limit in simple tension is 200
   N/mm2, determine whether the failure of the
   material will occur according to different failure
   theory. (take Poisson's ratio =0.3)
     Max principal strain theory
     Max shear stress theory
     Max strain energy theory
     Max shear strain energy theory

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Lecture 3 mohr’s circle and theory of failure

  • 2. Unit 1- Stress and Strain Topics Covered   Lecture -1 - Introduction, state of plane stress   Lecture -2 - Principle Stresses and Strains   Lecture -3 - Mohr's Stress Circle and Theory of Failure   Lecture -4- 3-D stress and strain, Equilibrium equations and impact loading   Lecture -5 - Generalized Hook's law and Castigliono's
  • 3. Mohr Stress Circle We derived these two equations- These equations represent the equation of a circle σ1 + σ2 σ1 − σ2 σn = + cos2θ + τ sin2θ 2 2 σ1 − σ2 σt = sin2θ − τ cos2θ 2 € ⎛ σ1 + σ2 ⎞ 2 ⎛ σ1 − σ2 ⎞ 2 ⎜σn − ⎟ = ⎜ cos2θ + τ sin2θ ⎟ € ⎝ 2 ⎠ ⎝ 2 ⎠ 2 ⎛ σ1 − σ2 ⎞ 2 (σt ) = ⎜ ⎝ 2 sin2θ − τ cos2θ ⎟ ⎠ €
  • 4. Mohr Stress Circle ⎛ σ1 + σ2 ⎞ 2 ⎛ σ1 − σ2 ⎞ 2 ⎜σn − ⎟ = ⎜ cos2θ + τ sin2θ ⎟ ⎝ 2 ⎠ ⎝ 2 ⎠ 2 ⎛ σ1 − σ2 ⎞ 2 (σt ) = ⎜ ⎝ 2 sin2θ − τ cos2θ ⎟ ⎠ Add above 2 equations. We will equation of circle. € 2 2 ⎛ σ + σ ⎞ 1 2 ⎛ σ − σ ⎞ 2 1 2 2 ⎜σ − n ⎟ + σ = ⎜ t ⎟ + (τ ) € ⎝ 2 ⎠ ⎝ 2 ⎠ 2 2 ( x − a) y r 2 Equation of circle €
  • 5. Mohr Stress Circle   Graphical method to determine stresses.   Body subjected to two mutually perpendicular principal stresses of unequal magnitude.   Body subjected to two mutually perpendicular principal stresses of unequal magnitude and unlike (one tensile and other compressive).   Body subjected to two mutually perpendicular principal stresses + simple shear stress.
  • 6. Mohr Stress Circle   Body subjected to two mutually perpendicular principal stresses of unequal magnitude (σ1 - σ2 ) length AD = Normal stress on oblique plane σt = σn E length ED = Tangential stress on Oblique plane = σt 2θ B length AE = Resultant stress on Oblique plane θ σn O D σ1 2 2 A C = σ +σt n € σ2 σ1 € €
  • 7. Mohr Stress Circle   Body subjected to two mutually perpendicular principal stresses of unequal magnitude and unlike (one tensile and other compressive). (σ1+σ2 ) length AD = Normal stress on oblique plane σt E = σn length ED = Tangential stress on Oblique plane = σt 2θ length AE = Resultant stress on Oblique plane C θ B σn 2 2 A O D = σt + σn _ € + σ1 σ2 € €
  • 8. Mohr Stress Circle   Body subjected to two mutually perpendicular principal stresses + simple shear stress. σt length AD = Normal stress on oblique plane = σn E length ED = Tangential stress on Oblique plane 2θ = σt length AE = Resultant stress on Oblique plane B M σ n L C D σ1 2 2 A O = σ +σ t n € σ2 σ1 € €
  • 9. Theories of failure   Maximum principal stress (Rankine theory)   Maximum principal strain (Saint Venant theory)   Maximum shear stress (Guest theory)   Maximum strain energy (Haigh theory)   Maximum shear strain energy (Mises & Henky theory)
  • 10. 1. Maximum principal stress theory σ1,σ2 ,σ3 =principal stresses in 3 perpendicular directions * max(σ1,σ2 ,σ3 ) ≤ σ € Maximum principal stress should be less than the max stress (yield stress) that material can bear in tension or compression. * σ = max tensile or compressive strength of material € σ* max principal stress= safety _ factor
  • 11. 2. Maximum principal strain theory σ1,σ2 ,σ3 =principal stresses in 3 perpendicular directions σ1 υσ2 υσ3 σ2 υσ1 υσ3 σ3 υσ1 υσ2 e1 = − − e2 = − − e3 = − − E E E E E E E E E * σ* € max(e1,e2 ,e3 ) ≤ e * e = E * σ = max tensile or compressive strength of material € Maximum principal strain should be less than the max strain (yield strain) that material € € can bear in tension or compression. € σ* € max principal stress= safety _ factor
  • 12. 3. Maximum shear stress theory max shear stress =half the difference of max and min principal stresses 1 = (σ1 − σ3 ) 2 In simple tension the stress To prevent failure max shear stress should be less that shear is existing in one direction stress in simple tension at elastic limit 1 * * = (σt − 0) σt max shear stress at elastic limit = max tensile of material € 2 (σ1 − σ 3 ) ≤ σ * t Maximum shear stress should be less than the max shear stress in simple tension (at elastic limit) that material can bear. € € σ*t allowable stress = € safety _ factor
  • 13. 4. Maximum strain energy theory Strain energy per unit volume should be less than the strain energy per unit volume in simple tension (at elastic limit) that material can bear. 2 [σ 2 1 + σ + σ − 2υ (σ1σ2 + σ1σ3 + σ2σ3 ) ≤ (σ 2 2 2 3 ] * t ) σ*t max allowable stress= safety _ factor € €
  • 14. 5. Maximum shear strain energy theory Shear strain energy per unit volume should be less than the shear strain energy per unit volume in simple tension (at elastic limit). 2 2 2 2 (σ1 − σ2 ) + (σ1 − σ3 ) + (σ2 − σ3 ) ≤ 2 * (σ * t ) σ*t max allowable stress= safety _ factor € €
  • 15. Important points   Brittle material -> Max principal stress   Brittle material do not fail in shear   Ductile material -> Max shear stress/max shear strain energy   Ductile material fail in shear because their yield strength is high.
  • 16. Failure Theory   PROBLEM- The principal stresses at a point in an elastic material are 200 N/mm2 (tensile), 100 N/ mm2 (tensile) and 50 N/mm2 (compressive). If the stresses at the elastic limit in simple tension is 200 N/mm2, determine whether the failure of the material will occur according to different failure theory. (take Poisson's ratio =0.3)   Max principal strain theory   Max shear stress theory   Max strain energy theory   Max shear strain energy theory