Unit 2- Stresses in Beams
Topics Covered
  Lecture -1 – Review of shear force and bending
   moment diagram

  Lecture -2 – Bending stresses in beams

  Lecture -3 – Shear stresses in beams

  Lecture -4- Deflection in beams

  Lecture -5 – Torsion in solid and hollow shafts.
Beam Deflection
Recall: THE ENGINEERING BEAM THEORY
                            σ M E
                              =   =
                            y   I   R
Moment-Curvature Equation

                     v (Deflection)
 y
                 €                                 NA
                                   A          B
     x




                                   A’         B’

If deformation is small (i.e. slope is “flat”):
1 dθ
                                                                      ∴ ≈
                                                                       R dx
               R
                                                    δy
                                  and      δθ ≈              (slope is “flat”)
                                                    δx
                       B’
                       δy           1 d2y                    €
  A’                               ⇒ ≈ 2
                                    R dx
                            €
          €
Alternatively: from Newton’s Curvature Equation

 y                      €                 ⎛ d 2 y ⎞               ⎛ dy ⎞ 2
           R                              ⎜ 2 ⎟                if ⎜ ⎟ <<<< 1
                                1         ⎝ dx ⎠                  ⎝ dx ⎠
                                  =                    3
               y = f (x)        R ⎛              2 ⎞ 2
                                         ⎛ dy ⎞
                                    ⎜1+ ⎜ ⎟ ⎟                  1 d2y
                   x                ⎝ ⎝ dx ⎠ ⎠                ⇒ ≈ 2
                                                         €         R dx
       €


                       €
From the Engineering Beam Theory:

                    M E           1 M   d2y
                      =            =   = 2
                    I   R         R EI  dx

                              d2y
                      ⇒ ( EI ) 2 = M
                              dx
      €Flexural       €          €            Bending
        Stiffness                             Moment
                            Curvature
          €
Relationship
A   C         B       Deflection = y
                                dy
                      Slope =
                                dx
                                             d2y
A   C         B       Bending moment = EI 2
        y                                    dx
                                          d3y
                      Shearing force = EI 3
                                         dx
                                           d4 y
                      Rate of loading = EI 4
                                           dx



                  €
Methods to find slope
       and deflection
  Double integration method

  Moment area method

  Macaulay’s method
Double integration method
                 d 2 y ⎛ 1 ⎞
                               ⎟ M                                 Curvature
    Since,           2 = ⎜
                 dx      ⎝ EI ⎠

               dy ⎛ 1 ⎞
             ⇒   = ⎜ ⎟ ∫ M ⋅ dx + C1                               Slope
               dx ⎝ EI ⎠
    €
                   ⎛ 1 ⎞
             ⇒ y = ⎜ ⎟ ∫     ∫ M ⋅ dx⋅ dx + ∫ C ⋅ dx + C
                                                 1           2        Deflection
                   ⎝ EI ⎠
€
        Where C1 and C2 are found using the boundary conditions.

€        Curvature                      Slope                    Deflection

                                                                      y
             R                           dy
                                         dx
Double integration method
Simple supported
            W
                                                 Slope             Deflection
        L/2                 L/2                      dy
A             C                     B      Slope =                Deflection = y c
                                                     dx
                      yc                                      2      WL3
                                                         WL       =−
                                           = θA = θB = −             48EI
                                                         16EI
                  L

Uniform distributed load

    x
                                   €             Slope
                                                     €
                                                                   Deflection
                           w/Unit length
A                 C                                  dy
                                    B      Slope =                Deflection = y c
                                                     dx
                      yc                                      2       5 WL3
                                                         WL       =−
                                           = θA = θB = −             384 EI
                                                         24 EI
                  L


                                                          €
                                   €
Macaulay’s method
  The procedure of finding slope and deflection for
   simply supported beam with an eccentric load is very
   laborious.

  Macaulay’s method helps to simplify the calculations
   to find the deflection of beams subjected to point
   loads.
Moment-Area Theorems
                             •  Consider a beam subjected to arbitrary
                                loading,
                                      dθ d 2 y M
                                        =     =
                                      dx dx 2 EI
                                      θD      xD
                                                   M
                                      ∫ dθ = ∫ EI dx
                                      θC      xC
                                                   xD
                                                        M
                                      θ D − θC =   ∫    EI
                                                           dx
                                                   xC
                    dx
                                      CD = Rdθ = dx
                              €
             €   R dθ

                             •  First Moment-Area Theorem:
         €
                                           area under BM diagram between
                         €                 C and D.
9 - 11
Moment-Area Theorems
                 •  Tangents to the elastic curve at P and P’
                    intercept a segment of length dt on the vertical
                    through C.
                                      M
                    dt = xdθ = x         dx
                                      EI
                             xD               x
                                    M       1 D          1 −
                    tC D =   ∫    x
                                    EI
                                       dx =     ∫ xMdx = EI A x
                                            EI xC
                             xC



                   −   A= total area of BM diagram between C & D
             €     x   = Distance of CG of BM diagram from C


                 •  Second Moment-Area Theorem:
                    The tangential deviation of C with respect to
         €          D is equal to the first moment with respect to
                    a vertical axis through C of the area under
                    the BM diagram between C and D.
9 - 12
Moment Area Method
Moment Area Method
An Exercise- Moment of Inertia – Comparison

1
               Load

                                                      Maximum distance of
                                                      4 inch to the centroid    I2

                      2 x 8 beam
                                                           Load                      2

                         I1



    Maximum distance of 1 inch to                                  2 x 8 beam
    the centroid


                        I2 > I1 , orientation 2 deflects less

    Ken Youssefi                    Engineering 10, SJSU                         15

Lecture 12 deflection in beams

  • 2.
    Unit 2- Stressesin Beams Topics Covered   Lecture -1 – Review of shear force and bending moment diagram   Lecture -2 – Bending stresses in beams   Lecture -3 – Shear stresses in beams   Lecture -4- Deflection in beams   Lecture -5 – Torsion in solid and hollow shafts.
  • 3.
    Beam Deflection Recall: THEENGINEERING BEAM THEORY σ M E = = y I R Moment-Curvature Equation v (Deflection) y € NA A B x A’ B’ If deformation is small (i.e. slope is “flat”):
  • 4.
    1 dθ ∴ ≈ R dx R δy and δθ ≈ (slope is “flat”) δx B’ δy 1 d2y € A’ ⇒ ≈ 2 R dx € € Alternatively: from Newton’s Curvature Equation y € ⎛ d 2 y ⎞ ⎛ dy ⎞ 2 R ⎜ 2 ⎟ if ⎜ ⎟ <<<< 1 1 ⎝ dx ⎠ ⎝ dx ⎠ = 3 y = f (x) R ⎛ 2 ⎞ 2 ⎛ dy ⎞ ⎜1+ ⎜ ⎟ ⎟ 1 d2y x ⎝ ⎝ dx ⎠ ⎠ ⇒ ≈ 2 € R dx € €
  • 5.
    From the EngineeringBeam Theory: M E 1 M d2y = = = 2 I R R EI dx d2y ⇒ ( EI ) 2 = M dx €Flexural € € Bending Stiffness Moment Curvature €
  • 6.
    Relationship A C B Deflection = y dy Slope = dx d2y A C B Bending moment = EI 2 y dx d3y Shearing force = EI 3 dx d4 y Rate of loading = EI 4 dx €
  • 7.
    Methods to findslope and deflection   Double integration method   Moment area method   Macaulay’s method
  • 8.
    Double integration method d 2 y ⎛ 1 ⎞ ⎟ M Curvature Since, 2 = ⎜ dx ⎝ EI ⎠ dy ⎛ 1 ⎞ ⇒ = ⎜ ⎟ ∫ M ⋅ dx + C1 Slope dx ⎝ EI ⎠ € ⎛ 1 ⎞ ⇒ y = ⎜ ⎟ ∫ ∫ M ⋅ dx⋅ dx + ∫ C ⋅ dx + C 1 2 Deflection ⎝ EI ⎠ € Where C1 and C2 are found using the boundary conditions. € Curvature Slope Deflection y R dy dx
  • 9.
    Double integration method Simplesupported W Slope Deflection L/2 L/2 dy A C B Slope = Deflection = y c dx yc 2 WL3 WL =− = θA = θB = − 48EI 16EI L Uniform distributed load x € Slope € Deflection w/Unit length A C dy B Slope = Deflection = y c dx yc 2 5 WL3 WL =− = θA = θB = − 384 EI 24 EI L € €
  • 10.
    Macaulay’s method   Theprocedure of finding slope and deflection for simply supported beam with an eccentric load is very laborious.   Macaulay’s method helps to simplify the calculations to find the deflection of beams subjected to point loads.
  • 11.
    Moment-Area Theorems •  Consider a beam subjected to arbitrary loading, dθ d 2 y M = = dx dx 2 EI θD xD M ∫ dθ = ∫ EI dx θC xC xD M θ D − θC = ∫ EI dx xC dx CD = Rdθ = dx € € R dθ •  First Moment-Area Theorem: € area under BM diagram between € C and D. 9 - 11
  • 12.
    Moment-Area Theorems •  Tangents to the elastic curve at P and P’ intercept a segment of length dt on the vertical through C. M dt = xdθ = x dx EI xD x M 1 D 1 − tC D = ∫ x EI dx = ∫ xMdx = EI A x EI xC xC − A= total area of BM diagram between C & D € x = Distance of CG of BM diagram from C •  Second Moment-Area Theorem: The tangential deviation of C with respect to € D is equal to the first moment with respect to a vertical axis through C of the area under the BM diagram between C and D. 9 - 12
  • 13.
  • 14.
  • 15.
    An Exercise- Momentof Inertia – Comparison 1 Load Maximum distance of 4 inch to the centroid I2 2 x 8 beam Load 2 I1 Maximum distance of 1 inch to 2 x 8 beam the centroid I2 > I1 , orientation 2 deflects less Ken Youssefi Engineering 10, SJSU 15