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Introduction to Acoustics

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a)<br />

b)<br />

Fig. 28.2a,b Two ways of representing a vibrational mode<br />

in a Korean pyeongyeong: (a) The shape at maximum<br />

bending; (b) The neutral shape with vec<strong>to</strong>rs<br />

timates by a second estimation process. The advantage<br />

of global curve fitting is that more-accurate frequency<br />

and damping estimates can potentially be obtained by<br />

processing all of the measurements rather than relying<br />

on a single measurement. Another advantage is that, because<br />

damping is already known and fixed as a result of<br />

the first step, the modal coefficients are more accurately<br />

estimated during the second step. Both the complex exponential<br />

and rational fraction polynomial methods can<br />

be formulated <strong>to</strong> obtain global estimates from a set of<br />

measurements [28.6].<br />

28.2.5 Real and Complex Modes<br />

The assumption of proportional viscous damping<br />

implies the existence of real, or normal modes. Mathematically,<br />

this implies that the damping matrix can<br />

be defined as a linear combination of the physical<br />

mass and stiffness matrices. Physically, all the<br />

points in a structure reach their maximum excursion,<br />

in one or the other direction, at the same time. The<br />

imaginary part of the FRF reaches a maximum at reso-<br />

28.3 Mathematical Modal Analysis<br />

In mathematical modal analysis, one attempts <strong>to</strong> uncouple<br />

the structural equation of motion by means<br />

of some suitable transformation, so that the un-<br />

Modal Analysis 28.3 Mathematical Modal Analysis 1133<br />

µm/s<br />

–500 0 500<br />

Fig. 28.3 Gray-scale representation of a vibration mode in<br />

a violin (courtesy of George Bissinger)<br />

nance, and the Nyquist circle lies along the imaginary<br />

axis.<br />

Some structures exhibit a more complicated form of<br />

damping, and the mode shapes are complex, meaning<br />

the phase angles can have values other than 0 or 180 ◦ .<br />

Different points on the structure reach their maxima at<br />

various times as in a traveling wave pattern. The imaginary<br />

part of the FRF no longer reaches a maximum at<br />

resonance nor is the real part zero. The Nyquist circle is<br />

rotated at an angle in the complex plane. When damping<br />

is light, the proportional damping assumption is generally<br />

an accurate approximation, [28.5] although it can<br />

be argued that a complex-mode formulation is essential<br />

<strong>to</strong> preserve accuracy in damping evaluation [28.7].<br />

28.2.6 Graphical Representation<br />

One of the nice features of experimental modal testing<br />

is the way that the modes can be represented graphically.<br />

Animations of the vibration can be viewed from<br />

any angle <strong>to</strong> comprehend complex mode shapes. Static<br />

representations include the shape at maximum bending,<br />

and the neutral shape with vec<strong>to</strong>rs, as shown in Fig. 28.2.<br />

Another representation is shown in Fig. 28.3.<br />

coupled equations can be solved. The frequency<br />

response of the structure can then be found by summing<br />

the respective modal responses in accordance<br />

Part H 28.3

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