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MODAL ANALYSIS - the Dept. of Mechanical Engineering at - Vrije ...

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The Frequency Response Function (FRF), denoted by H (ω)<br />

, is obtain by replacing <strong>the</strong> Laplace<br />

variable s in (4) by i ω resulting in<br />

1<br />

1<br />

H ( ω)<br />

= =<br />

(6)<br />

2<br />

2<br />

− mω<br />

+ icω<br />

+ k ( k − mω<br />

) + icω<br />

Clearly, if c = 0 , <strong>the</strong>n H (ω)<br />

goes to infinity for ω → ω k m (see Figure 4).<br />

Although very few practical structures could realistically be modeled by a single-degree-<strong>of</strong>-freedom<br />

(SDOF) system, <strong>the</strong> properties <strong>of</strong> such a system are important because those <strong>of</strong> a more complex<br />

multiple-degree-<strong>of</strong>-freedom (MDOF) system can always be represented as <strong>the</strong> linear superposition<br />

<strong>of</strong> a number <strong>of</strong> SDOF characteristics (when <strong>the</strong> system is linear time-invariant).<br />

2.2 Multiple Degree <strong>of</strong> Freedom<br />

Multiple-degree-<strong>of</strong>-freedom (MDOF) systems are described by <strong>the</strong> following equ<strong>at</strong>ion<br />

M x�<br />

�(<br />

t) + Cx�<br />

( t)<br />

+ Kx(<br />

t)<br />

= f(<br />

t)<br />

(7)<br />

In Figure 5, <strong>the</strong> different m<strong>at</strong>rices are defined for a 2-DOF system with both DOF along <strong>the</strong> vertical<br />

x-axis.<br />

f 1 (t)<br />

k 1<br />

f 2 (t)<br />

k 2<br />

m 2<br />

m 1<br />

c 2<br />

c 1<br />

x 2 (t)<br />

x 1 (t)<br />

⎡m<br />

M =<br />

⎢<br />

⎣<br />

1<br />

0<br />

n =<br />

⎡k1<br />

+ k<br />

K = ⎢<br />

⎣ − k2<br />

⎡c1<br />

+ c<br />

C = ⎢<br />

⎣ − c2<br />

0 ⎤<br />

m<br />

⎥<br />

2⎦<br />

2<br />

2<br />

− k<br />

k<br />

2<br />

− c<br />

Figure 5: 2-DOF system.<br />

c<br />

2<br />

⎤<br />

⎥<br />

⎦<br />

2<br />

⎤<br />

⎥<br />

⎦<br />

2<br />

⎧ f1(<br />

t)<br />

⎫<br />

f(<br />

t)<br />

= ⎨ ⎬<br />

⎩ f2(<br />

t)<br />

⎭<br />

⎧ x1(<br />

t)<br />

⎫<br />

x(<br />

t)<br />

= ⎨ ⎬<br />

⎩x2<br />

( t)<br />

⎭<br />

Transforming (7) to <strong>the</strong> Laplace domain (assuming zero initial conditions) yields<br />

Z( s) X(<br />

s)<br />

= F(<br />

s)<br />

(8)<br />

with Z (s)<br />

<strong>the</strong> dynamic stiffness m<strong>at</strong>rix<br />

2<br />

Z ( s)<br />

= Ms<br />

+ Cs<br />

+ K<br />

(9)<br />

The transfer function m<strong>at</strong>rix H (s)<br />

between displacement and force vectors, X ( s) = H(<br />

s)<br />

F(<br />

s)<br />

,<br />

equals <strong>the</strong> inverse <strong>of</strong> <strong>the</strong> dynamic stiffness m<strong>at</strong>rix<br />

2<br />

−1<br />

N(<br />

s)<br />

H ( s)<br />

= [ Ms<br />

+ Cs<br />

+ K]<br />

=<br />

d(<br />

s)<br />

with <strong>the</strong> numer<strong>at</strong>or polynomial m<strong>at</strong>rix N (s)<br />

given by<br />

2<br />

N ( s ) = adj(<br />

Ms<br />

+ Cs<br />

+ K)<br />

(11)<br />

and <strong>the</strong> common-denomin<strong>at</strong>or polynomial d (s)<br />

, also known as <strong>the</strong> characteristic polynomial,<br />

2<br />

d ( s)<br />

= det( M s + Cs<br />

+ K)<br />

(12)<br />

(10)

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