01 ce225 multi-degree of freedom systems

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  • 8/12/2019 01 CE225 Multi-Degree of Freedom Systems

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    Multi-Degree-of-Freedom Systems

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    Multi-Degree-of-Freedom Systems

    Degree-of-Freedom is two or more Degree-of-Freedom is the number of independent

    displacement coordinates necessary to describe the

    motion of the system.

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    k

    u

    m

    Examples of Single-Degree-of-Freedom Systems

    u

    k

    m

    u

    k

    m

    m

    k

    u

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    c1

    u1

    c2

    k1 k2

    m1 m2

    p1(t) p2(t)

    u2

    Examples of Two-Degree-of-Freedom Systems

    u1

    k1

    m1

    k2

    m2

    u2

    2-DOF

    2-DOF

    u1

    u2

    2-DOF

    Rigid bar

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    Example of Two-Degree-of-Freedom System

    k1

    k2

    m1

    m2

    u1

    u2

    2-DOF

    Shearbuilding

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    Example of Three-Degree-of-Freedom System

    c1

    u1

    c2 c3

    k1 k2 k3

    m1 m2 m3

    p1(t) p2(t) p3(t)

    u2 u3

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    Example of Three-Degree-of-Freedom System

    p1(t)

    p2(t)

    m1u1

    u2

    c1

    c2

    k1

    k2

    p3(t) u3

    k3

    m2

    m3

    c3

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    c1

    u1

    k1

    m1 m2

    p1(t) p2(t)

    u2

    Degree of Freedom does not necessarily mean the number

    of lumped masses

    u1

    k1

    m1

    m2

    u2

    1-DOF

    1-DOF

    Rigid bar

    u1 =u2

    Rigid bar

    u1 =u2

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    Equation of Motion of a Two-

    Degree-of-Freedom System

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    Two-Degree-of-Freedom Spring System (Classical)

    c1

    u1

    c2

    k1 k2

    m1 m2

    p1(t) p2(t)

    u2

    c1

    u1

    c2

    k1 k2

    m1 m2

    p1(t) p2(t)

    u2

    u1

    p1(t) p2(t)

    u2

    c1u1c2(u2-u1)

    k1u1 k2(u2-u1)

    c2(u2-u1)

    k2(u2-u1)

    m1u1 m1u1

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    Spring System

    u1

    p1(t)

    p2(t)

    u2

    c1u1 c2(u2-u1)

    k1u1 k2(u2-u1)

    c2(u2-u1)

    k2(u2-u1)

    m1u1

    m2u2

    m1u1+ + = p1(t)c1u1 k1u1c2(u2-u1)- k2(u2-u1)-

    m2u2+ + = p2(t)k2(u2-u1)c2(u2-u1)

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    Spring System

    c1

    u1

    m u(t) + c u(t) + k u(t) = p(t)

    c2

    k1 k2

    m1 m2

    p1(t) p2(t)

    u2

    Equation of Motion

    m1 0

    0 m2

    u1

    u2

    +

    c1+c2 -c2

    - c2 c2

    u1

    u2

    +

    k1+k2 -k2

    - k2 k2

    u1

    u2

    =

    p1(t)

    p2(t )

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    Spring System

    c1

    u1

    m v(t) + c v(t) + k v(t) = p(t)

    c2 c3

    k1 k2 k3

    m1 m2 m3

    p1(t) p2(t) p3(t)

    u2 u3

    Equation of Motion

    m1 0 0

    0 m2 0

    0 0 m3

    +

    c1+c2 -c2 0

    - c2 c2+c3 -c3

    0 -c3 c3

    +

    k1+k2 -k2 0

    - k2 k2+k3 -k3

    0 -k3 k3

    =

    p1(t)

    p2(t)

    p3(t )

    u1

    u2

    u3

    u1

    u2

    u3

    u1

    u2

    u3

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    Two-Story Shear Building

    (Assumptions)

    Beams and floor systems are rigid (infinitely stiff)

    in flexure

    Axial deformations of beams and columns are

    neglected Effect of axial force on stiffness of the columns

    are neglected

    Mass is concentrated at the floor levels Linear viscous damping is associated with

    deformational motions of each story

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    Two-Story Shear Building

    p1(t)

    p2(t)

    m1

    m2

    u1

    u2

    c1

    c2

    k1

    k2

    u2

    u1

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    Using Newtons Second Law of Motion

    p2(t)

    p1(t)

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    Using Newtons Second Law of Motion

    p2(t)

    p1(t)

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    Using Newtons Second Law of Motion

    p2(t)

    p1(t)

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    Using Newtons Second Law of Motion

    p2(t)

    p1(t)

    m2u2

    k2(u2-u1)

    k1u1 c1u1

    m2u2+ += p2(t)

    m1u1+ + = p1(t)

    m1u1

    c1u1 k1u1

    c2(u2-u1)

    k2(u2-u1) c2(u2-u1)

    k2(u2-u1)c2(u2-u1)

    c2(u2-u1)- k2(u2-u1)-

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    Using Newtons Second Law of Motion

    m2u2+ + =p2

    (t)

    m1u1+ + = p1(t)c1u1 k1u1

    k2(u2-u1)c2(u2-u1)

    c2(u2-u1)- k2(u2-u1)-

    m2u2- + =p2(t)k2u2c2u1 c2u2+ k2u1-

    m1u1+ - = p1(t)k2u2(c1+c2)u1 c2u2- + (k1+k2)u1

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    Using Newtons Second Law of Motion

    m2u2- + =p2(t)k2u2c2u1 c2u2+ k2u1-

    m1u1+ - = p1(t)k2u2(c1+c2)u1 c2u2- + (k1+k2)u1

    m1u1+ 0 u2 + (k1+k2)u1k2u2-(c1+c2)u1 c2u2-

    = p1(t)

    0 u1+ m2u2 - c2u1 + c2u2

    +

    k2u1- + k2u2= p2(t)

    m1 0

    0 m2

    u1

    u2

    +c1+c2 -c2

    - c2 c2

    u1

    u2

    +

    k1+k

    2-k2

    - k2 k2

    u1

    u2

    =

    p1(t)

    p2(t )

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    Using Newtons Second Law of Motion

    m1 0

    0 m2

    u1

    u2

    +

    c1+c2 -c2

    - c2 c2

    u1

    u2

    +

    k1+k2 -k2

    - k2 k2

    u1

    u2

    =

    p1(t)

    p2(t )

    m u+

    c u+

    k u = p(t)

    mass

    matr ix

    acc.

    vector

    damping

    matr ix

    vel.

    vector

    st i f fness

    matr ix

    disp.

    vector

    loading

    vector

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    Using Newtons Second Law of Motion

    m1 0

    0 m2

    u1

    u2

    +

    c1+c2 -c2

    - c2 c2

    u1

    u2

    +

    k1+k2 -k2

    - k2 k2

    u1

    u2

    =

    p1(t)

    p2(t )

    m u+

    c u+

    k u = p(t)

    This is the equation of motion of the two-story shear

    building

    The matrix equation represents two ordinary differential

    equations

    Each equation contains both u1 and u2, and, therefore,

    coupled.

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    General Form of the Equation of Motion

    m11 m12

    m21 m22

    u1

    u2

    +

    u1

    u2

    +

    u1

    u2

    =

    p1(t)

    p2(t )

    Physical meaning of each element of the matrices mij, cij, kijis the force at the i

    thmass due to a unit

    acceleration, velocity or displacement at the jthmass,

    respectively, with all other accelerations, velocities

    and displacements equal to zero.

    c11 c12

    c21 c22

    k11 k12

    k21 k22

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    Using Newtons Second Law of Motion

    p2(t)

    p1(t)

    m2u2

    k2(u2-u1)

    k1u1 c1u1

    m2u2+ += p2(t)

    m1u1+ + = p1(t)

    m1u1

    c1u1 k1u1

    c2(u2-u1)

    k2(u2-u1) c2(u2-u1)

    k2(u2-u1)c2(u2-u1)

    c2(u2-u1)- k2(u2-u1)-

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    Equation of Motion of a Three-

    Degree-of-Freedom System

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    Equation of Motion of a 3-DOF System

    m1 0 0

    0 m2 0

    0 0 m3

    u1

    u2

    u3

    +

    c1+c2 -c2 0

    - c2 c2+c3 -c3

    0 -c3 c3

    u1

    u2

    u3

    +

    k1+k2 -k2 0

    - k2 k2+k3 -k3

    0 -k3 k3

    u1

    u2

    u3

    =

    p1(t)

    p2(t)

    p3(t )

    p1(t)

    p2(t)

    m1u1

    u2

    c1

    c2

    k1

    k2

    p3(t) u3

    k3

    m2

    m3

    c3

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    Problem: Formulate the equation of motion of the given system.

    Level Weight (ton) Stiffness

    (ton/cm)

    5 100 53

    4 100 61.5

    3 100 96

    2 100 115

    1 100 114

    5

    4

    3

    2

    1

    m = W/g = W ton/980 cm/sec2

    100 0 0 0 0 y1 -115 -115 0 0 0 y1 0

    0 100 0 0 0 y2 -115 211 -96 0 0 y2 0

    0 0 100 0 0 y3 + 0 -96 157.5 -61.5 0 y3 = 0

    0 0 0 100 0 y40 0 -61.5 114.5 -53

    y4 00 0 0 0 100 y5 0 0 -53 53 y5 0

    1/980

    ton-sec2/cm cm ton/cmcm ton

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    Equation of Motion of a Two-

    Degree-of-Freedom System

    (Base Excitation, Undamped)

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    SDOF SystemOne-storey building with rigid girder

    (Influence of Support Excitation)

    fixedr

    eferen

    cea

    xis

    vg(t)

    vT(t)

    v(t)

    fs(t)

    2

    fs(t)

    2

    fD(t)

    fI(t)

    m

    k

    2

    k

    2fD(t)= c v(t)

    fs(t)= k v(t)

    fI(t)= m vT(t)

    F = 0 inertia force

    - fS(t) - fD(t) - fI(t) = 0

    - k v(t) - c v(t) - m (vg(t) + v(t) ) = 0

    m v(t)+ + k v(t) =c v(t) - m vg (t)

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    2-DOF SystemTwo-storey building with

    rigid girder (Influence of Support Excitation)

    fixedr

    eferencea

    xis

    vg

    v1T

    v1

    m1

    k

    2

    k

    2

    m2

    k

    2

    k

    2

    v2T

    v2

    Applications:

    1. Motion of building caused byearthquake

    2. Motion of equipment due tomotion of building where it ishoused

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    2-DOF SystemTwo-storey building with

    rigid girder (Influence of Support Excitation)

    = + v1

    disp of mass1 rel to

    moving support/base

    total disp of mass1 rel

    to fixed reference axis

    vgv1T

    disp of frame support

    rel to fixed reference

    axis

    fixedr

    eferencea

    xis

    vg

    v1T

    v1

    m1

    k

    2

    k

    2

    m2

    k

    2

    k

    2

    v2T

    v2

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    2-DOF SystemTwo-storey building with

    rigid girder (Influence of Support Excitation)

    = +

    disp of mass2 rel to

    moving support/base

    total disp of mass2 rel

    to fixed reference axis

    vgv2T

    disp of frame support

    rel to fixed reference

    axis

    fixedr

    eferencea

    xis

    vg

    v1T

    v1

    m1

    k

    2

    k

    2

    m2

    k

    2

    k

    2

    v2T

    v2

    v2

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    fixedr

    eferencea

    xis

    v

    m1 v1T

    k1v1

    v1

    v2

    v1)-k2(v2

    m2 v2T v1)-k2(v2+ = 0

    v1)-k2(v2

    m1 v1T+ k1v1 - v1)-k2(v2 = 0

    m2 v2T

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    vg displacement of support/ground from a fixed reference axis

    v1 displacement of mass1 relative to the base

    v2 displacement of mass2 relative to the base

    m2v2T v1)-k2(v2+ = 0

    m1v1T + k1v1 - v1)-k2 (v2 = 0

    = + v1vgv1T

    = +vgv2T v2

    v1 = + v1vgv1T

    = +vgv2T v2

    v1

    m2v2 k 2v2+k2v1- =

    m1v1 + (k1+ k2) v1 - k2 v2 = - m1vg

    - m2vg

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    m2v2 k 2v2+k2v1- =

    m1v1 + (k1+ k2) v1 - k2 v2 = -m1vg

    - m2vg

    m1

    0

    0

    m2

    +

    v1

    v2

    k1+k2

    - k2

    - k2

    k2

    v1

    v2= -

    m1

    0

    0

    m2

    1

    1

    vg

    M v + K v = - M 1 vg

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    Quiz

    m1

    0

    0

    m2

    +

    v1

    v2

    k1+k2

    - k2

    - k2

    k2

    v1

    v2= -

    m1

    0

    0

    m2

    1

    1

    vg

    MULTIPLY THE MATRICES

    2 x 2 2 x 1 2 x 2 2 x 1 2 x 2 2 x 1

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    Quiz

    m1

    0

    0

    m2

    +

    v1

    v2

    k1+k2

    - k2

    - k2

    k2

    v1

    v2= -

    m1

    0

    0

    m2

    1

    1

    vg

    MULTIPLY THE MATRICES

    ANSWER

    m1v1

    0 v1

    + 0 v2

    m2+ v2

    +( k1+k2 )v1 - k2v2

    - k2v1 + k2v2

    =

    - m1 vg

    - m2 vg

    2 x 1 2 x 1 2 x 1

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    QuizADD THE MATRICES

    m1v1

    0 v1

    + 0 v2

    m2+ v2

    +( k1+k2 )v1 - k2v2

    - k2v1 + k2v2

    =

    - m1 vg

    - m2 vg

    2 x 1 2 x 1 2 x 1

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    QuizADD THE MATRICES

    ANSWER

    m1v1

    0 v1

    + 0 v2

    m2+ v2

    +( k1+k2 )v1 - k2v2

    - k2v1 + k2v2

    =

    - m1 vg

    - m2 vg

    2 x 1 2 x 1 2 x 1

    m1v1+ 0 v2( k1+k2 )v1 - k2v2+

    0 v1 m2+ v2- k

    2 + k2v2

    2 x 1

    =

    - m1 vg

    - m2vg

    2 x 1

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    QuizWHAT ARE THE RESULTING TWO EQUATIONS?

    m1v1+ 0 v2( k1+k2 )v1 - k2v2+

    0 v1m2+ v2 - k2 + k2v2

    2 x 1

    =

    - m1 vg

    - m2 vg

    2 x 1

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    QuizWHAT ARE THE RESULTING TWO EQUATIONS?

    ANSWER

    m1v1+ 0 v2( k1+k2 )v1 - k2v2+

    0 v1m2+ v2 - k2 + k2v2

    2 x 1

    =

    - m1 vg

    - m2 vg

    2 x 1

    m1v1+ 0 v2( k1+k2 )v1 - k2v2+ = - m1 vg

    0 v1 m2+ v2 - k2 + k2v2 - m2 vg=

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    QuizCOMBINE THE TWO EQUATIONS INTO ONE MATRIX EQUATION

    m1v1( k1+k2 )v1 - k2v2+ = - m1 vg

    m2v2 - k2 + k2v2 - m2 vg=

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    QuizCOMBINE THE TWO EQUATIONS INTO ONE MATRIX EQUATION

    m1v1( k1+k2 )v1 - k2v2+ = - m1 vg

    m2v2 - k2 + k2v2 - m2 vg=

    ANSWER

    m1

    0

    0

    m2+

    v1

    v2

    k1+k2

    - k2

    - k2

    k2

    v1

    v2= -

    m1

    0

    0

    m2

    1

    1vg

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    k4= 1600 kN/mk4= 1600 kN/m

    k3= 1200 kN/mk3= 1200 kN/m

    m4= 4500 kg

    k2= 800 kN/mk2= 800 kN/m

    m3= 3000 kg

    m2= 3000 kg

    k1= 400 kN/mk1= 400 kN/m

    m1= 1500 kg

    x1

    x2

    x3

    x4

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    k4= 1600 kN/mk4= 1600 kN/m

    k3= 1200 kN/mk3= 1200 kN/m

    m4= 4500 kg

    k2= 800 kN/mk2= 800 kN/m

    m3= 3000 kg

    m2= 3000 kg

    k1= 400 kN/mk1= 400 kN/m

    m1= 1500 kgx1

    x2

    x3

    x4

    x1=1

    x2=0

    x3=0

    x4=0

    800 kN

    800 kN

    800 kN

    - 800 kN

    0

    0

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    k4= 1600 kN/mk4= 1600 kN/m

    k3= 1200 kN/mk3= 1200 kN/m

    m4= 4500 kg

    k2= 800 kN/mk2= 800 kN/m

    m3= 3000 kg

    m2= 3000 kg

    k1= 400 kN/mk1= 400 kN/m

    m1= 1500 kgx1

    x2

    x3

    x4

    x1=0

    x2=1

    x3=0

    x4=0

    800 kN

    800 kN

    1600 kN

    1600 kN

    - 800 kN

    2400 kN

    - 1600

    0

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    k4= 1600 kN/mk4= 1600 kN/m

    k3= 1200 kN/mk3= 1200 kN/m

    m4= 4500 kg

    k2= 800 kN/mk2= 800 kN/m

    m3= 3000 kg

    m2= 3000 kg

    k1= 400 kN/mk1= 400 kN/m

    m1= 1500 kg

    x1

    x2

    x3

    x4

    x1=0

    x3=1

    x2=0

    x4=0

    1600 kN

    1600 kN

    2400 kN

    2400 kN

    0

    - 1600 kN

    4000 kN

    -2400 kN

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    k4= 1600 kN/mk4= 1600 kN/m

    k3= 1200 kN/mk3= 1200 kN/m

    m4= 4500 kg

    k2= 800 kN/mk2= 800 kN/m

    m3= 3000 kg

    m2= 3000 kg

    k1= 400 kN/mk1= 400 kN/m

    m1= 1500 kg

    x1

    x2

    x3

    x4

    x1=0

    x4=1

    x2=0

    x3=0

    2400 kN

    2400 kN

    3200 kN

    3200 kN

    0

    0

    -2400 kN

    5600 kN

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    800

    - 800

    0

    0

    - 800

    2400

    - 1600

    0

    0

    - 1600

    4000

    -2400

    0

    0

    -2400

    5600

    F1

    F2

    F3

    F4

    =

    x1

    x2

    x3

    x4

    1 2 3 4

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    1500

    0

    0

    0

    0

    3000

    0

    0

    0

    0

    3000

    0

    0

    0

    0

    4500

    F1

    F2

    F3

    F4

    =

    x1

    x2

    x3

    x4

    1 2 3 4

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    0

    0

    x4

    1500

    0

    0

    0

    0

    3000

    0

    0

    0

    0

    3000

    0

    0

    0

    0

    4500

    x1

    x2

    x3

    x4

    1 2 3 4

    +

    800

    - 800

    0

    0

    - 800

    2400

    - 1600

    0

    0

    - 1600

    4000

    -2400

    0

    0

    -2400

    5600

    x1

    x2

    x3

    1 2 3 4

    =0

    0

    M x + K x = 0

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    M x + K x = 0

    Equation of motion:

    Let x = a sin ( t )

    x = a sin ( t )- 2

    (a)

    (b)

    Substitute (b) to (a) results in

    K - 2 Ma = 0

    =12

    .

    .

    n

    a1 =a11a21

    .

    .

    an1

    a2 =a12a22

    .

    .

    an2

    etc.

    Mode1 Mode2

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    END