determination of natural frequencies-analytical methods

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    Determination of naturalFrequencies-Analytical Method

    • Dunkerley’s Formula

    • Rayleigh’s Method

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    • Expansion of characteristic determinant and the solution of the res

    degree polynomial to get natural frequencies is tedious for large vaDOF (n).

    • These methods will give approximate value (s) of natural frequenc

    mode shapes

    Preamble

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    • Gives approximate value of fundamental frequency of a composite

    terms of natural frequencies of its component parts.

    • Derived from the fact that the higher natural frequencies of most vi

    systems are large compared to their fundamental frequencies.

    • Frequency equation

    I - [k] +2 I = 0 (

    I - 

    [I] +   I = 0 where [a] is flexibility matrix (

    Dunkerley’s Formula

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    For a lumped mass system with a diagonal mass matrix, (1) becomes

    I - 

    1 ⋯ 0⋮ ⋱ ⋮0 ⋯ 1

    +

      ⋯ ⋮ ⋱ ⋮

      ⋯

      ⋯ 0⋮ ⋱ ⋮0 ⋯

    I = 0

    I

    −  

     +   ⋯

    ⋮ ⋱ ⋮

      ⋯ − 

     +

    I = 0 (3

    Dunkerley’s Formula

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    The expansion of equation (3) leads to

    n

    -    + 222 + … .

    n-1

    ....= 0

    Polynomial of nth degree in

    . Let the roots of (4) be denoted by

    Thus

     −

     

     −

     

    ….

     −

     

    =

    n -

     

     + 

     + … 

    n-1

    Equating coefficients of

    n-1 in (4) and (5)

     +

     

     + …

     

    =  + 222 + … .

    Dunkerley’s Formula

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    In most cases, the higher frequencies 2 , 3 … are considerably

    than fundamental frequency

    ,

    ∴ 

     ≪

     

    , I = 2,3….n

    ∴ Equation (6) can be written approximately as

     ≅  + 222 + … . (

    • Fundamental frequency given by (7) is always smaller than the ex

    Dunkerley’s Formula

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    Estimate the fundamental frequency of a simply supported beam car

    identical equally spaced masses.

    Problem 1

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    Rayleigh’s Principal:

    • The frequency of vibration of a conservative system vibrating about

    equilibrium position has a stationary value in the neighborhood of amode. This stationary value, in fact, is a minimum value in the neighof the fundamental natural mode.

    • The PE and KE of the n-DOF system is

    V =

    2 {} [k] {} (8)

    T =

    2 { ሶ}

    [m] { ሶ} (9)•  Assume harmonic solution

    x = X cos (10)

    X- mode shape vector / modal vector,

    - natural frequency of vibration

    Rayleigh’s Method

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    If the system is conservative, the maximum KE = maximum PE

    Tmax = Vmax (12)

    Substituting (10) in (8 and 9) and simplifying

    Tmax =

    2 [m]   2

    Vmax =

    2 [k]  

    Equating

    2=

    [k]   [m]   (13) Rayleigh

    Rayleigh’s Method

    Rayleigh’s quotient provides an upper bound for2

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    Procedure:

    1. Select a trial vector X to represent the first natural mode X1 and sRHS of (13).

    2. Calculate 2

    3. If the trial vector is more closer to first natural mode X1 , value of

    more accurate

    Rayleigh’s Method

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    Estimate the fundamental frequency of vibration of 

    the system shown in Figure. Assume that for  

    k1=k2=k3=k, m1=m2=m3=m , and the modeshape is X = { 1 2 3}T

    Problem 2

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