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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.
Why study stresses in
      beams
What are beams
  A structural member which is long when compared
   with its lateral dimensions, subjected to transverse
   forces so applied as to induce bending of the
   member in an axial plane, is called a beam.
Objective
  When a beam is loaded by forces or couples,
   stresses and strains are created throughout the
   interior of the beam.

  To determine these stresses and strains, the
   internal forces and internal couples that act on the
   cross sections of the beam must be found.
Beam Types
  Types of beams- depending on how they are
   supported.
    
Load Types on Beams
  Types of loads on beam
     Concentrated or point load


     Uniformly distributed load


     Uniformly varying load


     Concentrated Moment
Sign Convention for
          forces and moments
                  P       M                M



                              Q        Q




“Happy” Beam is +VE

                      +VE (POSITIVE)
Sign Convention for
          forces and moments
                        M                M


           P

                            Q        Q




“Sad” Beam is -VE

                    -VE (POSITIVE)
Sign Convention for
     forces and moments
  Positive directions are denoted by an internal shear
   force that causes clockwise rotation of the member
   on which it acts, and an internal moment that
   causes compression, or pushing on the upper arm
   of the member.

  Loads that are opposite to these are considered
   negative.
SHEAR FORCES AND BENDING
           MOMENTS
  The resultant of the stresses must be such as to
   maintain the equilibrium of the free body.

  The resultant of the stresses acting on the cross
   section can be reduced to a shear force and a
   bending moment.

  The stress resultants in statically determinate
   beams can be calculated from equations of
   equilibrium.
Shear Force and Bending
  Moment in a Beam
Shear Force and Bending
          Moment
  Shear Force:      is the algebraic sum of the vertical
   forces acting to the left or right of the cut section



  Bending Moment: is the algebraic sum of the
   moment of the forces to the left or to the right of the
   section taken about the section
SF and BM formulas
Cantilever with point load
                             W
                        x        Fx= Shear force at X
      A                          Mx= Bending Moment at X
                             B


               L


W                  SF             Fx=+W



          BM                      Mx=-Wx
WxL
                                  at x=0=> Mx=0
                                  at x=L=> Mx=-WL
SF and BM formulas
  Cantilever with uniform distributed load
            w Per unit
            length       x                   Fx= Shear force at X
                                             Mx= Bending Moment at X
        A                       B


                  L
                                              Fx=+wx
             BM                               at x=0 Fx=0
  wL                                          at x=L Fx=wL


                                    Mx=-(total load on right portion)*
                                    Distance of C.G of right portion
wL2/2                               Mx=-(wx).x/2=-wx2/2
                                    at x=0=> Mx=0
                                    at x=L=> Mx=-wl2/2
SF and BM formulas
  Cantilever with gradually varying load

                                               Fx= Shear force at X
   w                       wx/L
                                               Mx= Bending Moment at X
       A                            B
                            x
                                                         wx 2
                L                                   Fx =
                                                         2L
                                                    at x=0 Fx=0
                                                    at x=L Fx=wL/2
wL/2                                    €
                                Parabola
                       C
                                        Mx=-(total load for length x)*
                                        Distance of load from X
                                             wx 3
                    Cubic               Mx =
                                             6L
                                        at x=0=> Mx=0
                                        at x=L=> Mx=-wl2/6
                                €
SF and BM formulas
     Simply supported with point load

                        W
                  x                                   Fx= Shear force at X
                            C
                                                      Mx= Bending Moment at X
          A                                B
             W                                    W
      RA =
             2         L                   RB =
                                                  2

                                                       Fx=+W/2 (SF between A & C)
€                                  €                   Resultant force on the left portion
    W/2           SF
                                Baseline B             ⎛ W    ⎞    W      Constant force
             A         C                               ⎜ − W ⎟ = −
                                                       ⎝ 2    ⎠    2      between B to C
                                 SF        W/2


                                                  €
                  BM
                       WL/4

              B         C              B
SF and BM formulas
     Simply supported with point load

                        W
                  x                              Fx= Shear force at X
                            C
                                                 Mx= Bending Moment at X
          A                           B
             W                               W
      RA =             L              RB = for section
             2                               2
                                           between A & C
                                                        W
€                            €             M x = RA x =     x
    W/2           SF                                    2
                          Baseline B       at A x=0=> MA=0 W L
             A        C                    at C x=L/2=> MC =            ×
                            SF      W/2                               2 2
                                    €       for section
                                            between C & B
                  BM                               €W × ⎛ x − L ⎞ = W x − Wx + W L
                                        M x = RA x −     ⎜      ⎟
                     WL/4                                ⎝    2 ⎠ 2              2
                                            W         L
              B        C          B     = − x +W
                                             2        2
                                               WL W
                                        MB =       − L =0
                                                2     2
                                  €
SF and BM formulas
  Simply supported with uniform distributed load
             w Per unit length
              x                           Fx= Shear force at X
                                          Mx= Bending Moment at X
        A                        B

        RA                  C    RB
                      L
                                                      wL
                                          RA = RB =
                 BM                                    2
  wL/2                                                    wL
                                          Fx = RA − w.x =      − w.x
        A                 C      B                         2
                                                       wL w.0 wL
                                          x = 0 ⇒ FA =      −      =
                                 wL/2                   2       2     2
                                              L        wL wL
                                          x = ⇒ FC =         −     =0
                      wL2                     2          2      2
wL2/2
                       8                               wL            wL
                                          x = L ⇒ FB =      − wL =
                                                        2             2


             €
                                 €
SF and BM formulas
  Simply supported with uniform distributed load
             w Per unit length
              x                                Fx= Shear force at X
                                               Mx= Bending Moment at X
        A                           B

                            C                             x
        RA                          RB M x = RA x − w.x
                      L                                   2
                                          wL    w.x 2
                 BM                     =    x−
  wL/2                                     2     2
        A                 C         B                wL      w.0
                                        x = 0 ⇒ MA =    .0 −     =0
                                                      2       2
                                 wL/2       L
                                                                    2
                                                     wL L w ⎛ L ⎞ wL2 wL2 wL2
                                        x = ⇒ Mc =       . − ⎜ ⎟ =    −   =
                                            2         2 2 2 ⎝ 2 ⎠   4   8   8
wL2/2                 wL2
                                                     wL      w
                       8                x = L ⇒ MB =     L − L2 = 0
                                                      2      2


             €
                                €
SF and BM diagram
            P       Constant     Linear
 Load


         Constant    Linear     Parabolic
Shear


          Linear    Parabolic    Cubic
Moment
SF and BM diagram
              0        0       Constant
 Load     M




         Constant   Constant    Linear
Shear


          Linear     Linear    Parabolic
Moment
Relation between load, shear
     force and bending moment
                1        2
        x                    w/m run
                                                     dF
A                                      B                = −w
                                                     dx
                1 C      2
            L                              The rate of change of shear force is equal
                                           to the rate of loading
            M            M+dM              €
    F                        F+dF                    dM
                    dx                                    =F
                                                      dx
                                           The rate of change of bending moment
                                           is equal to the shear force at the section
                                           €

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Lecture 9 shear force and bending moment in beams

  • 1.
  • 2. 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.
  • 4. What are beams   A structural member which is long when compared with its lateral dimensions, subjected to transverse forces so applied as to induce bending of the member in an axial plane, is called a beam.
  • 5. Objective   When a beam is loaded by forces or couples, stresses and strains are created throughout the interior of the beam.   To determine these stresses and strains, the internal forces and internal couples that act on the cross sections of the beam must be found.
  • 6. Beam Types   Types of beams- depending on how they are supported.  
  • 7. Load Types on Beams   Types of loads on beam   Concentrated or point load   Uniformly distributed load   Uniformly varying load   Concentrated Moment
  • 8. Sign Convention for forces and moments P M M Q Q “Happy” Beam is +VE +VE (POSITIVE)
  • 9. Sign Convention for forces and moments M M P Q Q “Sad” Beam is -VE -VE (POSITIVE)
  • 10. Sign Convention for forces and moments   Positive directions are denoted by an internal shear force that causes clockwise rotation of the member on which it acts, and an internal moment that causes compression, or pushing on the upper arm of the member.   Loads that are opposite to these are considered negative.
  • 11. SHEAR FORCES AND BENDING MOMENTS   The resultant of the stresses must be such as to maintain the equilibrium of the free body.   The resultant of the stresses acting on the cross section can be reduced to a shear force and a bending moment.   The stress resultants in statically determinate beams can be calculated from equations of equilibrium.
  • 12. Shear Force and Bending Moment in a Beam
  • 13. Shear Force and Bending Moment   Shear Force: is the algebraic sum of the vertical forces acting to the left or right of the cut section   Bending Moment: is the algebraic sum of the moment of the forces to the left or to the right of the section taken about the section
  • 14. SF and BM formulas Cantilever with point load W x Fx= Shear force at X A Mx= Bending Moment at X B L W SF Fx=+W BM Mx=-Wx WxL at x=0=> Mx=0 at x=L=> Mx=-WL
  • 15. SF and BM formulas Cantilever with uniform distributed load w Per unit length x Fx= Shear force at X Mx= Bending Moment at X A B L Fx=+wx BM at x=0 Fx=0 wL at x=L Fx=wL Mx=-(total load on right portion)* Distance of C.G of right portion wL2/2 Mx=-(wx).x/2=-wx2/2 at x=0=> Mx=0 at x=L=> Mx=-wl2/2
  • 16. SF and BM formulas Cantilever with gradually varying load Fx= Shear force at X w wx/L Mx= Bending Moment at X A B x wx 2 L Fx = 2L at x=0 Fx=0 at x=L Fx=wL/2 wL/2 € Parabola C Mx=-(total load for length x)* Distance of load from X wx 3 Cubic Mx = 6L at x=0=> Mx=0 at x=L=> Mx=-wl2/6 €
  • 17. SF and BM formulas Simply supported with point load W x Fx= Shear force at X C Mx= Bending Moment at X A B W W RA = 2 L RB = 2 Fx=+W/2 (SF between A & C) € € Resultant force on the left portion W/2 SF Baseline B ⎛ W ⎞ W Constant force A C ⎜ − W ⎟ = − ⎝ 2 ⎠ 2 between B to C SF W/2 € BM WL/4 B C B
  • 18. SF and BM formulas Simply supported with point load W x Fx= Shear force at X C Mx= Bending Moment at X A B W W RA = L RB = for section 2 2 between A & C W € € M x = RA x = x W/2 SF 2 Baseline B at A x=0=> MA=0 W L A C at C x=L/2=> MC = × SF W/2 2 2 € for section between C & B BM €W × ⎛ x − L ⎞ = W x − Wx + W L M x = RA x − ⎜ ⎟ WL/4 ⎝ 2 ⎠ 2 2 W L B C B = − x +W 2 2 WL W MB = − L =0 2 2 €
  • 19. SF and BM formulas Simply supported with uniform distributed load w Per unit length x Fx= Shear force at X Mx= Bending Moment at X A B RA C RB L wL RA = RB = BM 2 wL/2 wL Fx = RA − w.x = − w.x A C B 2 wL w.0 wL x = 0 ⇒ FA = − = wL/2 2 2 2 L wL wL x = ⇒ FC = − =0 wL2 2 2 2 wL2/2 8 wL wL x = L ⇒ FB = − wL = 2 2 € €
  • 20. SF and BM formulas Simply supported with uniform distributed load w Per unit length x Fx= Shear force at X Mx= Bending Moment at X A B C x RA RB M x = RA x − w.x L 2 wL w.x 2 BM = x− wL/2 2 2 A C B wL w.0 x = 0 ⇒ MA = .0 − =0 2 2 wL/2 L 2 wL L w ⎛ L ⎞ wL2 wL2 wL2 x = ⇒ Mc = . − ⎜ ⎟ = − = 2 2 2 2 ⎝ 2 ⎠ 4 8 8 wL2/2 wL2 wL w 8 x = L ⇒ MB = L − L2 = 0 2 2 € €
  • 21. SF and BM diagram P Constant Linear Load Constant Linear Parabolic Shear Linear Parabolic Cubic Moment
  • 22. SF and BM diagram 0 0 Constant Load M Constant Constant Linear Shear Linear Linear Parabolic Moment
  • 23. Relation between load, shear force and bending moment 1 2 x w/m run dF A B = −w dx 1 C 2 L The rate of change of shear force is equal to the rate of loading M M+dM € F F+dF dM dx =F dx The rate of change of bending moment is equal to the shear force at the section €