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
Stresses and strains
    In last lecture we looked at stresses were acting in a
      plane that was at right angles/parallel to the action of
      force.
Tensile Stress                                Shear Stress
Stresses and strains
  Compressive load                                          Failure in shear




Stresses are acting normal to the surface yet the material failed in a different plane
Principal stresses and
            strains
  What are principal stresses.
     Planes that have no shear stress are called as principal
       planes.
     Principal planes carry only normal stresses
Stresses in oblique plane
  In real life stresses does not act in normal direction but
   rather in inclined planes.

   Normal Plane                         Oblique Plane
Stresses in oblique plane
                                               P
                                            σ=
             θ                                 A
                                      P =Axial Force
                                      A=Cross-sectional area
                                      perpendicular to force
    €                                                  2
        σn       Unit depth
                                  €    σn = σ cos θ
                                            σ
€                                      σt = sin2θ
                                            2
        σt                    €

€                             €
Stresses in oblique plane
                                                                   σ1                                 σ1
    Member subjected to direct stress in one plane

                                                                                             σ2
                                                      €                                     €
    Member subjected to direct stress in two mutually             σ1                                 σ1
     perpendicular plane
                                                                        €
                                                                                            σ2
                                                                                τ
                                                      €                                     €
                                                                    τ                                 τ
    Member subjected to simple shear stress.
                                                          €             €               τ
                                                                                    σ2 €          τ
                                                      €
                                                                                                      τ
    Member subjected to direct stress in two                 σ1                                       σ1
                                                                   €
     mutually perpendicular directions + simple shear         τ
     stress                                                                         €
                                                              €
                                                                            τ               σ
                                                                                            €2
                                                 €                                          €
                                                 €
                                                          €             €
Stresses in oblique plane
          Member subjected to direct stress in two mutually
           perpendicular directions + simple shear stress


                σ1 + σ2 σ1 − σ2
           σn =         +        cos2θ + τ sin2θ
                   2         2
                     σ1 − σ2
                σt =         sin2θ − τ cos2θ
                        2
€

    €
Stresses in oblique plane
      Member subjected to direct stress in two mutually
       perpendicular directions + simple shear stress
         POSITION OF PRINCIPAL PLANES
            Shear stress should be zero


                σ1 − σ2
           σt =         sin2θ − τ cos2θ = 0
                   2
                             2τ
                  tan2θ =
                           σ1 − σ2
€
Stresses in oblique plane
      Member subjected to direct stress in two mutually
        perpendicular directions + simple shear stress
          POSITION OF PRINCIPAL PLANES

              2τ
    tan2θ =
            σ1 − σ 2
                    2τ                                     2τ
    sin2θ =              2
              (σ1 − σ 2 ) + 4τ 2                 θ
€
    cos2θ =
                 (σ1 − σ 2 )                    σ1 − σ 2
                         2
              (σ1 − σ 2 ) + 4τ 2               €
€
                                    €

€                                   €
Stresses in oblique plane
    Member subjected to direct stress in two mutually
      perpendicular directions + simple shear stress
                                                  2
                           σ1 + σ2   ⎛ σ1 − σ2 ⎞
Major principal Stress   =         + ⎜         ⎟ +τ2
                              2      ⎝ 2 ⎠

                                                  2
                           σ1 + σ2   ⎛ σ1 − σ2 ⎞     2
Minor principal Stress   =         − ⎜         ⎟ + τ
          €                   2      ⎝ 2 ⎠



          €
Stresses in oblique plane
      Member subjected to direct stress in two mutually
       perpendicular directions + simple shear stress
         MAX SHEAR STRESS

                          d
                         dθ
                            (σ t ) = 0
      d   ⎡σ1 − σ 2           ⎤                      σ1 − σ 2
          ⎢ 2 sin2θ − τ cos2θ ⎥ = 0          tan2θ =
     dθ   ⎣                   ⎦                        2τ
              €

€
                                   €
Stresses in oblique plane
          Member subjected to direct stress in two mutually
           perpendicular directions + simple shear stress
             MAX SHEAR STRESS

            Evaluate the following equation at
                 σ1 − σ2
            σt =         sin2θ − τ cos2θ
                    2
                    σ1 − σ 2
            tan2θ =
                      2τ
                         1                       2
€          (σt )max    =
                         2
                                (σ1 − σ2 ) + 4τ 2
    €
Stresses in oblique plane
  Member subjected to direct stress in one plane

  Member subjected to direct stress in two mutually
   perpendicular plane

  Member subjected to simple shear stress.

  Member subjected to direct stress in two mutually
   perpendicular directions + simple shear stress
Stresses in oblique plane
          Member subjected to direct stress in one plane

                  σ1 + σ2 σ1 − σ2
             σn =         +        cos2θ + τ sin2θ
                     2         2
                       σ1 − σ2
                  σt =         sin2θ − τ cos2θ
                          2
        Stress in one direction and no shear stress   σ2 = 0 τ = 0
€
                        σ1 σ1
                    σn = + cos2θ = σ1 cos2 θ
    €                   2 2
                            € σ €
                               1
                          σt = sin2θ
                              2
    €
Stresses in oblique plane
          Member subjected to direct stress in two mutually
             perpendicular plane

                  σ1 + σ2 σ1 − σ2
             σn =         +        cos2θ + τ sin2θ
                     2         2
                       σ1 − σ2
                  σt =         sin2θ − τ cos2θ
                          2
        Stress in two direction and no shear stress   τ =0
€
                                σ1 + σ2 σ1 − σ2
                           σn =         +        cos2θ
    €                              2          2
                                 €σ − σ
                             σt = 1      2
                                           sin2θ
                                      2
         €
Stresses in oblique plane
          Member subjected to simple shear stress.


                  σ1 + σ2 σ1 − σ2
             σn =         +        cos2θ + τ sin2θ
                     2         2
                       σ1 − σ2
                  σt =         sin2θ − τ cos2θ
                          2
        No stress in axial direction but only shear stress   σ1 = σ 2 = 0
€
                                     σn = τ sin2θ
    €                                σt = € τ cos2θ
                                          −

                   €
                   €
Principal stresses and
           strains
  PROBLEM- The tensile stresses at a point across
   two mutually perpendicular planes are 120N/mm2
   and 60 N/mm2. Determine the normal, tangential
   and resultant stresses on a plane inclined at 30deg to
   the minor stress.
Principal stresses and
            strains
  PROBLEM- A rectangular block of material is
   subjected to a tensile stress of 110 N/mm2 on one
   plane and a tensile stress of 47 N/mm2 on the plane
   at right angles to the former. Each of the above
   stresses is accompanied by a shear stress of 63 N/
   mm2 and that associated with the former tensile
   stress tends to rotate the block anticlockwise. Find

1)The direction and magnitude of each of the principal
   stress.

2) Magnitude of the greatest shear stress.

Lecture 2 principal stress and strain

  • 2.
    Unit 1- Stressand 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.
    Stresses and strains   In last lecture we looked at stresses were acting in a plane that was at right angles/parallel to the action of force. Tensile Stress Shear Stress
  • 4.
    Stresses and strains Compressive load Failure in shear Stresses are acting normal to the surface yet the material failed in a different plane
  • 5.
    Principal stresses and strains   What are principal stresses.   Planes that have no shear stress are called as principal planes.   Principal planes carry only normal stresses
  • 6.
    Stresses in obliqueplane   In real life stresses does not act in normal direction but rather in inclined planes. Normal Plane Oblique Plane
  • 7.
    Stresses in obliqueplane P σ= θ A P =Axial Force A=Cross-sectional area perpendicular to force € 2 σn Unit depth € σn = σ cos θ σ € σt = sin2θ 2 σt € € €
  • 8.
    Stresses in obliqueplane σ1 σ1   Member subjected to direct stress in one plane σ2 € €   Member subjected to direct stress in two mutually σ1 σ1 perpendicular plane € σ2 τ € € τ τ   Member subjected to simple shear stress. € € τ σ2 € τ € τ   Member subjected to direct stress in two σ1 σ1 € mutually perpendicular directions + simple shear τ stress € € τ σ €2 € € € € €
  • 9.
    Stresses in obliqueplane   Member subjected to direct stress in two mutually perpendicular directions + simple shear stress σ1 + σ2 σ1 − σ2 σn = + cos2θ + τ sin2θ 2 2 σ1 − σ2 σt = sin2θ − τ cos2θ 2 € €
  • 10.
    Stresses in obliqueplane   Member subjected to direct stress in two mutually perpendicular directions + simple shear stress   POSITION OF PRINCIPAL PLANES   Shear stress should be zero σ1 − σ2 σt = sin2θ − τ cos2θ = 0 2 2τ tan2θ = σ1 − σ2 €
  • 11.
    Stresses in obliqueplane   Member subjected to direct stress in two mutually perpendicular directions + simple shear stress   POSITION OF PRINCIPAL PLANES 2τ tan2θ = σ1 − σ 2 2τ 2τ sin2θ = 2 (σ1 − σ 2 ) + 4τ 2 θ € cos2θ = (σ1 − σ 2 ) σ1 − σ 2 2 (σ1 − σ 2 ) + 4τ 2 € € € € €
  • 12.
    Stresses in obliqueplane   Member subjected to direct stress in two mutually perpendicular directions + simple shear stress 2 σ1 + σ2 ⎛ σ1 − σ2 ⎞ Major principal Stress = + ⎜ ⎟ +τ2 2 ⎝ 2 ⎠ 2 σ1 + σ2 ⎛ σ1 − σ2 ⎞ 2 Minor principal Stress = − ⎜ ⎟ + τ € 2 ⎝ 2 ⎠ €
  • 13.
    Stresses in obliqueplane   Member subjected to direct stress in two mutually perpendicular directions + simple shear stress   MAX SHEAR STRESS d dθ (σ t ) = 0 d ⎡σ1 − σ 2 ⎤ σ1 − σ 2 ⎢ 2 sin2θ − τ cos2θ ⎥ = 0 tan2θ = dθ ⎣ ⎦ 2τ € € €
  • 14.
    Stresses in obliqueplane   Member subjected to direct stress in two mutually perpendicular directions + simple shear stress   MAX SHEAR STRESS Evaluate the following equation at σ1 − σ2 σt = sin2θ − τ cos2θ 2 σ1 − σ 2 tan2θ = 2τ 1 2 € (σt )max = 2 (σ1 − σ2 ) + 4τ 2 €
  • 15.
    Stresses in obliqueplane   Member subjected to direct stress in one plane   Member subjected to direct stress in two mutually perpendicular plane   Member subjected to simple shear stress.   Member subjected to direct stress in two mutually perpendicular directions + simple shear stress
  • 16.
    Stresses in obliqueplane   Member subjected to direct stress in one plane σ1 + σ2 σ1 − σ2 σn = + cos2θ + τ sin2θ 2 2 σ1 − σ2 σt = sin2θ − τ cos2θ 2 Stress in one direction and no shear stress σ2 = 0 τ = 0 € σ1 σ1 σn = + cos2θ = σ1 cos2 θ € 2 2 € σ € 1 σt = sin2θ 2 €
  • 17.
    Stresses in obliqueplane   Member subjected to direct stress in two mutually perpendicular plane σ1 + σ2 σ1 − σ2 σn = + cos2θ + τ sin2θ 2 2 σ1 − σ2 σt = sin2θ − τ cos2θ 2 Stress in two direction and no shear stress τ =0 € σ1 + σ2 σ1 − σ2 σn = + cos2θ € 2 2 €σ − σ σt = 1 2 sin2θ 2 €
  • 18.
    Stresses in obliqueplane   Member subjected to simple shear stress. σ1 + σ2 σ1 − σ2 σn = + cos2θ + τ sin2θ 2 2 σ1 − σ2 σt = sin2θ − τ cos2θ 2 No stress in axial direction but only shear stress σ1 = σ 2 = 0 € σn = τ sin2θ € σt = € τ cos2θ − € €
  • 19.
    Principal stresses and strains   PROBLEM- The tensile stresses at a point across two mutually perpendicular planes are 120N/mm2 and 60 N/mm2. Determine the normal, tangential and resultant stresses on a plane inclined at 30deg to the minor stress.
  • 20.
    Principal stresses and strains   PROBLEM- A rectangular block of material is subjected to a tensile stress of 110 N/mm2 on one plane and a tensile stress of 47 N/mm2 on the plane at right angles to the former. Each of the above stresses is accompanied by a shear stress of 63 N/ mm2 and that associated with the former tensile stress tends to rotate the block anticlockwise. Find 1)The direction and magnitude of each of the principal stress. 2) Magnitude of the greatest shear stress.