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Title: Stress Transformation 9.1-9.3 Plane Stress Stress


1
Stress Transformation
  • 9.1-9.3
  • Plane Stress
  • Stress Transformation in Plane Stress
  • Principal Stresses Maximum Shear Stress

2
Introduction
  • We have learned
  • Axially
  • In Torsion
  • In bending
  • These stresses act on cross sections of the
    members.
  • Larger stresses can occur on inclined sections.

3
Introduction
  • We will look at stress elements to analyze the
    state of stress produce by a single type of load
    or by a combination of loads.
  • From the stress element, we will derive the
    Transformation Equations
  • Give the stresses acting on the sides of an
    element oriented in a different direction.

4
Introduction
  • Stress elements only one intrinsic state of
    stress exists at a point in a stressed body,
    regardless of the orientation of the element for
    that state of stress.
  • Two elements with different orientations at the
    same point in a body, the stress acting on the
    faces of the two elements are different, but
    represent the same state of stress
  • The stress at the point under consideration.

5
Introduction
  • Remember, stresses are not vectors.
  • Are represented like a vector with magnitude and
    direction
  • Do not combine with vector algebra
  • Stresses are much more complex quantities than
    vectors
  • Are called Tensors (like strain and I)

6
Plane Stress
  • Plane Stress The state of stress when we
    analyzed bars in tension and compression, shafts
    in torsion, and beams in bending.
  • Consider a 3 dimensional stress element
  • Material is in plane stress in the xy plane
  • Only the x and y faces of the element are
    subjected to stresses
  • All stresses act parallel to the x and y axis

7
Plane Stress
  • Normal stress
  • subscript identifies the face on which the stress
    acts
  • Sign Convention
  • Tension positive
  • compression negative

8
Plane Stress
  • Shear Stress -
  • Two subscripts
  • First denotes the face on which the stress acts
  • Second gives the direction on that face
  • Sign convention
  • Positive when acts on a positive face of an
    element in the positive direction of an axis ()
    or (--)
  • Negative when acts on a positive face of an
    element in the negative direction of an axis (-)
    or (-)

9
Plane Stress
  • A 2-dimensional view can depict the relevant
    stress information, fig. 9.1c
  • Special cases
  • Uniaxial Stress
  • Pure shear
  • Biaxial stress

10
Stresses on Inclined Planes
  • First we know ?x, ?y, and ?xy,
  • Consider a new stress element
  • Located at the same point in the material as the
    original element, but is rotated about the z axis
  • x and y axis rotated through an angle ?

11
Stresses on Inclined Planes
  • The normal and shear stresses acting on they new
    element are
  • Using the same subscript designations and sign
    conventions described.
  • Remembering equilibrium, we know that

12
Stresses on Inclined Planes
  • The stresses in the xy plane can be expressed
    in terms of the stresses on the xy element by
    using equilibrium.
  • Consider a wedge shaped element
  • Inclined face same as the x face of inclined
    element.

13
Stresses on Inclined Planes
  • Construct a FBD showing all the forces acting on
    the faces
  • The sectioned face is ?A.
  • Then the normal and shear forces can be
    represented on the FBD.
  • Summing forces in the x and y directions and
    remembering trig identities, we get

14
Stresses on Inclined Planes
  • These are called the transformation equations for
    plane stress.
  • They transfer the stress component form one set
    of axes to another.
  • The state of stress remains the same.
  • Based only on equilibrium, do not depend on
    material properties or geometry
  • There are Strain Transformation equations that
    are based solely on the geometry of deformation.

15
Stresses on Inclined Planes
  • Special case simplifications
  • Uniaxial stress- ?y Txy 0
  • Pure Shear - ?x ?y 0
  • Biaxial stress - Txy 0
  • Transformation equations are simplified
    accordingly.

16
Principal Maximum Shear Stresses
  • Since a structural member can fail due to
    excessive normal or shear stress, we need to know
    what the maximum normal and stresses are at a
    point.
  • We will determine the maximum and minimum stress
    planes for which maximum and minimum normal and
    shear stresses act.

17
Principal Maximum Shear Stresses
  • Principal stresses maximum and minimum normal
    stresses.
  • Occurs on planes where
  • Applying to eq 9.1 we get
  • ?pthe orientation of the principal planes
  • The planes on which the principal stresses act.

18
Principal Maximum Shear Stresses
  • Two values of the angle 2?p are obtained from the
    equation.
  • One value 0-180, other 180-360
  • Therefore ?p has two values 0-90 90-180
  • Values are called Principal Angles.
  • For one angle ?x is maximum, the other ?x is
    minimum.
  • Therefore Principal stresses occur on mutually
    perpendicular planes.

19
Principal Maximum Shear Stresses
  • We could find the principal stress by
    substituting this angle into the transformation
    equation and solving
  • Or we could derive general formulas for the
    principal stresses.

20
Principal Stresses
  • Consider the right triangle
  • Using the trig from the triangle and substituting
    into the transformation equation for normal
    stress, we get
  • Formula for principal stresses.

21
Shear Stresses on the Principal Planes
  • If we set the shear stress ?xy equal to zero in
    the transformation equation and solve for 2?, we
    get equation 9-4.
  • The angles to the planes of zero shear stress are
    the same as the angles to the principal planes
  • ThereforeThe shear stresses are zero on the
    principal planes

22
The Third Principal Stress
  • We looked only at the xy plane rotating about the
    z-axis.
  • Equations derived are in-plane principal stresses
  • BUT, stress element is 3D and has 3 principal
    stresses.
  • By Eigenvalue analysis it can be shown that ?z0
    when oriented on the principal plane.

23
Maximum In-Plane Shear Stress
  • Consider the maximum shear stress and the plane
    on which they act.
  • The shear stresses are given by the
    transformation equations.
  • Taking the derivative of ?xy with respect to ?
    and setting it equal to zero we can derive
    equation 9-7

24
Maximum Shear Stress
  • The maximum negative shear stress ?min has the
    same magnitude but opposite sign.
  • The planes of maximum shear stress occur at 45 to
    the principal planes

25
Maximum Shear Stress
  • If we use equation 9-5, subtract ?2 from ?1, and
    compare with equation 9-7, we see that
  • Maximum shear stress is equal to ½ the difference
    of the principal shear stress.

26
Average Normal Stress
  • The planes of maximum shear stress also contain
    normal stresses.
  • Normal stresses acting on the planes of maximum
    positive shear stress can be determined by
    substituting the expressions for the angle ?s
    into the equations for ?x.
  • Result is Equation 9-8.

27
Important Points
  • The principal stresses are the max and min normal
    stress at a point
  • When the state of stress is represented by the
    principal stresses, no shear stress acts on the
    element
  • The state of stress at the point can also be
    represented in terms of max in-plane shear
    stress. In this case an average normal stress
    also acts on the element
  • The element in max in-plane shear stress is
    oriented 45 from the element in principal
    stresses.

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