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7 Transformations of Stress and Strain
Transformations of Stress and Strain ,[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object],[object Object]
Introduction ,[object Object],[object Object],[object Object]
Introduction ,[object Object],[object Object],[object Object]
Transformation of Plane Stress ,[object Object],[object Object]
Principal Stresses ,[object Object],[object Object]
Maximum Shearing Stress Maximum shearing stress  occurs for
Example 7.01 For the state of plane stress shown, determine (a) the principal panes, (b) the principal stresses, (c) the maximum shearing stress and the corresponding normal stress. ,[object Object],[object Object],[object Object],[object Object]
Example 7.01 ,[object Object],[object Object],[object Object]
Example 7.01 ,[object Object],[object Object]
Sample Problem 7.1 A single horizontal force  P  of 150 lb magnitude is applied to end D of lever  ABD .  Determine (a) the normal and shearing stresses on an element at point  H  having sides parallel to the  x  and  y  axes, (b) the principal planes and principal stresses at the point  H . ,[object Object],[object Object],[object Object],[object Object]
Sample Problem 7.1 ,[object Object],[object Object],[object Object]
Sample Problem 7.1 ,[object Object]
Mohr’s Circle for Plane Stress ,[object Object],[object Object],[object Object],The direction of rotation of  Ox  to  Oa  is the same as  CX  to  CA .
Mohr’s Circle for Plane Stress ,[object Object],[object Object],[object Object]
Mohr’s Circle for Plane Stress ,[object Object],[object Object]
Example 7.02 For the state of plane stress shown, (a) construct Mohr’s circle, determine (b) the principal planes, (c) the principal stresses, (d) the maximum shearing stress and the corresponding normal stress. ,[object Object],[object Object]
Example 7.02 ,[object Object]
Example 7.02 ,[object Object]
Sample Problem 7.2 For the state of stress shown, determine (a) the principal planes and the principal stresses, (b) the stress components exerted on the element obtained by rotating the given element counterclockwise through 30 degrees. ,[object Object],[object Object]
Sample Problem 7.2 ,[object Object]
Sample Problem 7.2 ,[object Object],[object Object]
General State of Stress ,[object Object],[object Object],[object Object],[object Object],[object Object],These are the principal axes and principal planes and the normal stresses are the principal stresses.
Application of Mohr’s Circle to the Three- Dimensional Analysis of Stress ,[object Object],[object Object],[object Object],[object Object]
Application of Mohr’s Circle to the Three- Dimensional Analysis of Stress ,[object Object],[object Object],[object Object],[object Object],[object Object]
Application of Mohr’s Circle to the Three- Dimensional Analysis of Stress ,[object Object],[object Object],[object Object],[object Object]
Yield Criteria for Ductile Materials Under Plane Stress ,[object Object],[object Object],[object Object],[object Object]
Yield Criteria for Ductile Materials Under Plane Stress Maximum shearing stress criteria: Structural component is safe as long as the maximum shearing stress is less than the maximum shearing stress in a tensile test specimen at yield, i.e., For   a  and   b  with the same sign, For   a  and   b  with opposite signs,
Yield Criteria for Ductile Materials Under Plane Stress Maximum distortion energy criteria: Structural component is safe as long as the distortion energy per unit volume is less than that occurring in a tensile test specimen at yield.
Fracture Criteria for Brittle Materials Under Plane Stress Maximum normal stress criteria: Structural component is safe as long as the maximum normal stress is less than the ultimate strength of a tensile test specimen. Brittle materials fail suddenly through rupture or fracture in a tensile test.  The failure condition is characterized by the ultimate strength   U .
Stresses in Thin-Walled Pressure Vessels ,[object Object],[object Object],[object Object]
Stresses in Thin-Walled Pressure Vessels ,[object Object],[object Object],[object Object]
Stresses in Thin-Walled Pressure Vessels ,[object Object],[object Object],[object Object]
Transformation of Plane Strain ,[object Object],[object Object],[object Object]
Transformation of Plane Strain ,[object Object],[object Object]
Mohr’s Circle for Plane Strain ,[object Object],[object Object],[object Object],[object Object]
Three-Dimensional Analysis of Strain ,[object Object],[object Object],[object Object]
Three-Dimensional Analysis of Strain ,[object Object],[object Object],[object Object],[object Object],[object Object]
Three-Dimensional Analysis of Strain ,[object Object],[object Object],[object Object],[object Object]
Measurements of Strain: Strain Rosette ,[object Object],[object Object],[object Object]

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7 stress transformations

  • 1. 7 Transformations of Stress and Strain
  • 2.
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  • 7. Maximum Shearing Stress Maximum shearing stress occurs for
  • 8.
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  • 21.
  • 22.
  • 23.
  • 24.
  • 25.
  • 26.
  • 27.
  • 28. Yield Criteria for Ductile Materials Under Plane Stress Maximum shearing stress criteria: Structural component is safe as long as the maximum shearing stress is less than the maximum shearing stress in a tensile test specimen at yield, i.e., For  a and  b with the same sign, For  a and  b with opposite signs,
  • 29. Yield Criteria for Ductile Materials Under Plane Stress Maximum distortion energy criteria: Structural component is safe as long as the distortion energy per unit volume is less than that occurring in a tensile test specimen at yield.
  • 30. Fracture Criteria for Brittle Materials Under Plane Stress Maximum normal stress criteria: Structural component is safe as long as the maximum normal stress is less than the ultimate strength of a tensile test specimen. Brittle materials fail suddenly through rupture or fracture in a tensile test. The failure condition is characterized by the ultimate strength  U .
  • 31.
  • 32.
  • 33.
  • 34.
  • 35.
  • 36.
  • 37.
  • 38.
  • 39.
  • 40.