4.SDOF Systems in Free Vibration

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  • 8/2/2019 4.SDOF Systems in Free Vibration

    1/5

    Free vibration response due to initial conditions

    J. Enrique Martinez-Rueda Dynamics of Structures 1

    Solution to the equation of motion of a SDOF systemunder free vibration

    If there is no excitation force then the equation of motion of a SDOF system becomes:

    0)()()( *** =++ t Y K t Y C t Y M &&& (fv.1)

    The above equation of motion is a 2 nd degree differential equation with constantcoefficients; the solution of the equation is the displacement response ) (t Y , if this isassumed to be:

    t Aet Y =)( (fv.2)Then the velocity and the acceleration responses will be given as:

    t e Adt

    t dY t Y == )()(& (fv.3)

    t e Adt

    t Y d t Y 2)()( ==

    &&& (fv.4)

    Substituting the above functions ) (t Y , )(t Y & and )(t Y && in the equation of motion (fv.1)

    0**2* =++ t t t AeK e AC e A M (fv.5)

    Dividing everything by t Ae

    0**2* =++ K C M characteristic equation (fv.6)

    The solution to this equation is

    2*

    **2

    *

    *

    *

    *

    *

    **2**

    4

    4

    222

    4

    M

    K M

    M

    C

    M

    C

    M

    K M C C

    == (fv.7)

    or

    *

    *2

    *

    *

    *

    *

    22 M

    K

    M

    C

    M

    C

    = (fv.8)

    But if we change the variables of eqn (fv.8) using:

    *

    *

    M

    K = [rad/sec] = undamped circular frequency (fv.9)

    *

    *

    2 M

    C = = damping ratio (fv.10)

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    Free vibration response due to initial conditions

    J. Enrique Martinez-Rueda Dynamics of Structures 2

    Then eqn. (fv.8) can be rewritten as:

    12222 == (fv.11)

    Now, there are three possibilities for

    case 1 . =1.0 i.e., critically damped system

    = 1 = 2 = - (i.e., the two values of are equal) (fv.12)

    The Theory of Differential Equations (TED) shows that, in this case, the solution is:

    t t teC eC t Y 21)( += (fv.13)

    or t t teC eC t Y +=21

    )( (fv.14)

    or ( )t C eC t Y t 21 1)( += (fv.15)

    case 2. > 1.0 i.e ., overdamped system

    1 2 and TED shows the solution is:t t eC eC t Y 21 21)(

    += (fv.16)or

    +

    +=1

    2

    1

    1

    22

    )( t t

    eC eC t Y (fv.17)

    case 3. < 1.0 i.e. , underdamped system

    Now the term 12 is imaginary and hence 1 and 2 are complex numbers

    222 1111 == i (fv.18)

    2

    1 = i (fv.19) or d i = (fv.20)

    where 21 =d [rad/sec] damped circular frequency ( d < ) (fv.21)

    Finally, TED shows that the solution in this case is:

    ( )t C t C et Y d d t sincos)( 21 += (fv.22)

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    Free vibration response due to initial conditions

    J. Enrique Martinez-Rueda Dynamics of Structures 3

    Physical interpretation of the above solutions

    1. systems with critical damping ( = 1)

    0.0 0.1 0.2 0.3 0.4 0.50.0

    0.2

    0.4

    0.6

    0.8

    1.0

    =1

    t

    Y(t)

    2. overdamped systems ( > 1)

    0.0 0.1 0.2 0.3 0.4 0.50.0

    0.5

    1.0

    1.5

    2.0

    > 1

    t

    Y(t)

    In both of the above cases:

    the displacement response Y(t) is characterised by exponential decay with nooscillation

    in general the theory of systems with 1 is used for the design of shock absorvers or damping mechanisms of doors.

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    Free vibration response due to initial conditions

    J. Enrique Martinez-Rueda Dynamics of Structures 4

    3. underdamped systems ( < 1)

    Td

    Y(t)

    t

    infinite number of oscillations (in theory) amplitude of oscillations decay in an exponential fashion

    in conventional structures is typically assumed to be 2-5% but in specialstructures it can be as high as 20%

    the system vibrates at the damped frequency d with a damped period T d :

    d

    d T 2= [sec] (fv.23)

    For systems with no damping, we define:

    2=T [sec] = natural period or period of vibration (fv.24)

    2

    1 ==T

    f [Hertz = cycles/sec ] = natural frequency (fv.25)

    The natural period can be seen as the time required by the system to complete a fullcycle of vibration .

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    Free vibration response due to initial conditions

    J. Enrique Martinez-Rueda Dynamics of Structures 5

    Response of damped SDOF system in free vibration dueto initial conditions

    The displacement response of this system is given by:

    ( )t C t C et Y d d t sincos)( 21 += (fv.26)

    where C 1 & C 2 are integration constants that can be found invoking the initial i.e . boundaryconditions of the problem.

    Deriving the above eqn. with respect to time we get

    ( ) ( )t C t C et C t C et Y d d d t

    d d d d t

    sincoscossin)( 2121 ++=

    & (fv.27)

    Now, let us assume we know the initial conditions (initial displacement Y o and initialvelocity oY

    &) of the response Y(t):

    Y o = Y (0) at t = 0 (fv.28)

    )0(Y Y o&& = at t = 0 (fv.29)

    Substituting the above initial conditions into eqns (fv.26) and (fv.27) we get:

    Y o = 1 ( C 1 + 0) Y o = C 1 (fv.30)

    =oY & 1(-0 + C 2 d ) - C 1

    d

    oo Y Y C +=

    &2 (fv.31)

    Hence the displacement response of the system will be:

    ++= t Y Y t Y et Y d

    d

    ood ot sincos)(

    &(fv.32)

    It can be shown that if the initial conditions are invoked for time 0 thenthe response of the system is given by:

    ( ) ( ) ( ) ( ) ( ) ( )

    ++=

    t Y Y t Y et Y d d

    d t sincos)(

    &(fv.33)