lecture6 shear force and bending moment in beams

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  • 7/30/2019 Lecture6 Shear Force and Bending Moment in Beams

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  • 7/30/2019 Lecture6 Shear Force and Bending Moment in Beams

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    Unit 2- Stresses in Beams

    Lecture -1 Review of shear force and bendingmoment 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.

    Topics Covered

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    Why study stresses in

    beams

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    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.

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    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, theinternal forces and internal couples that act on the

    cross sections of the beam must be found.

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    Beam Types Types of beams- depending on how they are

    supported.

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    Load Types on Beams Types of loads on beam

    Concentrated or point load

    Uniformly distributed load

    Uniformly varying load

    Concentrated Moment

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    P

    Happy Beam is +VE

    +VE (POSITIVE)

    M M

    Q Q

    Sign Convention for

    forces and moments

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    -VE (POSITIVE)

    M M

    Q Q

    Sign Convention for

    forces and moments

    Sad Beam is -VE

    P

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    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 thatcauses compression, or pushing on the upper arm

    of the member.

    Loads that are opposite to these are considerednegative.

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    SHEAR FORCES AND BENDING

    MOMENTS

    The resultant of the stresses must be such as tomaintain the equilibrium of the free body.

    The resultant of the stresses acting on the crosssection can be reduced to a shear force and a

    bending moment.

    The stress resultants in statically determinatebeams can be calculated from equations ofequilibrium.

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    Shear Force and Bending

    Moment in a Beam

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    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 themoment of the forces to the left or to the right of thesection taken about the section

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    SF and BM formulas

    B

    L

    x

    A

    W

    SFW

    WxL BM

    Fx= Shear force at X

    Mx= Bending Moment at X

    Fx=+W

    Mx=-Wxat x=0=> Mx=0at x=L=> Mx=-WL

    Cantilever with point load

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    SF and BM formulas

    B

    L

    x

    A

    wLBM

    Fx= Shear force at X

    Mx= Bending Moment at X

    Fx=+wx

    at x=0 Fx=0at x=L Fx=wL

    Mx=-(total load on right portion)*Distance of C.G of right portionMx=-(wx).x/2=-wx

    2/2

    at x=0=> Mx=0

    at x=L=> Mx=-wl2/2

    w Per unit

    length

    wL2/2

    Cantilever with uniform distributed load

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    SF and BM formulas

    B

    L

    x

    A

    Fx= Shear force at X

    Mx= Bending Moment at X

    at x=0 Fx=0

    at x=L Fx=wL/2

    Mx=-(total load for length x)*Distance of load from X

    at x=0=> Mx=0

    at x=L=> Mx=-wl2/6

    wL/2

    Cantilever with gradually varying load

    w wx/L

    C

    Fx =wx

    2

    2L

    Mx=

    wx3

    6L

    Parabola

    Cubic

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    SF and BM formulas

    B

    L

    x

    A

    W

    SFW/2

    WL/4BM

    Fx= Shear force at X

    Mx= Bending Moment at X

    Fx=+W/2 (SF between A & C)Resultant force on the left portion

    Simply supported with point load

    RA=

    W

    2

    RB=

    W

    2

    C

    SF W/2

    BaselineA C

    B

    BCB

    W

    2W

    =

    W

    2

    Constant force

    between B to C

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    SF and BM formulas

    B

    L

    x

    A

    W

    SFW/2

    WL/4BM

    Fx= Shear force at X

    Mx= Bending Moment at X

    at A x=0=> MA=0

    at C x=L/2=>

    Simply supported with point load

    RA=

    W

    2

    RB=

    W

    2

    C

    SF W/2

    BaselineA C

    B

    BCB

    Mx= R

    Ax =

    W

    2x

    MC=

    W

    2L

    2

    for section

    between A & C

    Mx= R

    Ax W x

    L

    2

    =

    W

    2x Wx +W

    L

    2

    = W

    2x +W

    L

    2

    for section

    between C & B

    MB=

    WL

    2

    W

    2

    L = 0

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    SF and BM formulas

    B

    L

    x

    A

    wL/2BM

    Fx= Shear force at X

    Mx= Bending Moment at X

    w Per unit length

    wL2/2

    Simply supported with uniform distributed load

    CRA RB

    wL/2

    C BA

    wL2

    8

    RA

    = RB

    =

    wL

    2

    Fx= R

    Aw.x =

    wL

    2w.x

    x = 0 FA

    =

    wL

    2w.0

    2=

    wL

    2

    x =L

    2 F

    C=

    wL

    2wL

    2= 0

    x = L FB

    =

    wL

    2wL =

    wL

    2

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    SF and BM formulas

    B

    L

    x

    A

    wL/2BM

    Fx= Shear force at X

    Mx= Bending Moment at X

    w Per unit length

    wL2/2

    Simply supported with uniform distributed load

    CRA RB

    wL/2

    C BA

    wL2

    8

    Mx= R

    Ax w.x

    x

    2

    =

    wL

    2x

    w.x2

    2

    x = 0 MA

    =

    wL

    2.0

    w.0

    2= 0

    x =L

    2 Mc =

    wL

    2.L

    2w

    2

    L

    2

    2

    =

    wL2

    4wL

    2

    8=

    wL2

    8

    x = L MB

    =

    wL

    2L

    w

    2L

    2= 0

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    Load

    P Constant Linear

    Shear

    Constant Linear Parabolic

    Moment

    Linear Parabolic Cubic

    SF and BM diagram

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    Load

    0 0 Constant

    Shear

    Constant Constant Linear

    Moment

    Linear Linear Parabolic

    M

    SF and BM diagram

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    Relation between load, shear

    force and bending moment

    B

    L

    x

    AC

    1

    1 2

    2

    dx

    F+dFF

    w/m run

    dF

    dx= w

    dM

    dx= F

    The rate of change of shear force is equalto the rate of loading

    The rate of change of bending moment

    is equal to the shear force at the section

    M+dMM