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Introduction to Acoustics

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922 Part G Structural <strong>Acoustics</strong> and Noise<br />

Part G 22.4<br />

which yields the equation of the eigenfrequencies<br />

(Fig. 22.11)<br />

cos ωL ωL<br />

cosh = 1 . (22.162)<br />

c c<br />

The numerical resolution of (22.162) shows that the<br />

eigenfrequencies fn (in Hz) are<br />

fn ≈<br />

�<br />

EI π<br />

ρS 8L 2<br />

�<br />

3.011 2 , 5 2 , 7 2 ,... ,(2n + 1) 2�<br />

.<br />

(22.163)<br />

The eigenfrequencies are not harmonically related so<br />

that the impulse response of the beam is not periodic.<br />

Beam with a Variable Cross Section<br />

As another example, we consider the flexural vibrations<br />

for a beam with variable cross section. Here, we describe<br />

the Galerkin method [22.12]. It has the advantage<br />

that it remains valid even in the case of nonconservative<br />

systems. In this method, the eigenfunctions Φ(x)of<br />

(22.154) are approximated by a finite sum of p terms<br />

Φ (p) p�<br />

(x) = a jφ j(x) , (22.164)<br />

j=1<br />

where φ j(x) are arbitrary functions that satisfy the<br />

boundary conditions at both ends of the beam. Inserting<br />

(22.164) in(22.154), and defining λ (p) = (ω2 ) (p) as<br />

the approximate eigenvalues of order p, one can define<br />

the Galerkin residue<br />

�<br />

R Φ (p) �<br />

(x) = d2<br />

dx2 �<br />

EI(x) d2Φ (p)<br />

dx2 �<br />

− λ (p) ρ(x)S(x)Φ (p)<br />

following (22.164), this can be written as<br />

�<br />

R Φ (p) � p�<br />

(x) = a j ×<br />

j=1<br />

(22.165)<br />

�<br />

d2 dx2 �<br />

EI(x) d2φ j(x)<br />

dx2 �<br />

− λ (p) �<br />

ρ(x)S(x)φ j(x) .<br />

(22.166)<br />

The weak formulation of the problem is given by<br />

�L<br />

p�<br />

�<br />

d2 φi(x) a j<br />

dx<br />

0<br />

j=1<br />

2<br />

�<br />

EI(x) d2φ j(x)<br />

dx2 �<br />

− λ (p) �<br />

ρ(x)S(x)φ j(x) dx = 0 . (22.167)<br />

The goal of the method is <strong>to</strong> find the coefficients a j for<br />

which the residue R � Φ (p) (x) � is equal <strong>to</strong> zero. Thus<br />

(22.167) becomes<br />

p�<br />

kija j − λ (p)<br />

p�<br />

mija j = 0<br />

j=1<br />

kij =<br />

0<br />

j=1<br />

for i = 1, 2,...p , (22.168)<br />

where the mass and stiffness coefficients are<br />

�L<br />

φi(x) d2<br />

dx2 �<br />

EI(x) d2φ j(x)<br />

dx2 �<br />

dx (22.169)<br />

and<br />

�<br />

L<br />

mij =<br />

0<br />

φi(x)ρ(x)S(x)φ j(x) dx . (22.170)<br />

Equation (22.168) can be written equivalently in matrix<br />

form:<br />

[K − λM] a = 0 , (22.171)<br />

where a is a vec<strong>to</strong>r with dimension p and K and M<br />

are matrices with dimension p × p. The problem <strong>to</strong> be<br />

solved is therefore equivalent in form <strong>to</strong> the eigenvalue<br />

problem for a p-component discrete system (22.49).<br />

Prestressed Beam or Stiff String<br />

The flexural motion for a beam subjected <strong>to</strong> tension<br />

(or prestressed beam) is governed by the same equation<br />

as a string with stiffness. For a homogeneous and<br />

isotropic beam of constant section subjected <strong>to</strong> a uniform<br />

tension T,wehave<br />

ρS ∂2v ∂t2 = T ∂2v ∂x2 − EI∂4 v<br />

. (22.172)<br />

∂x4 For a propagating wave of the form y(x, t) = ei(ωt−kx) ,<br />

we obtain the dispersion relationship<br />

ω 2 = k 2 c 2<br />

�<br />

1 + EI<br />

T k2<br />

�<br />

. (22.173)<br />

For a stiff string of length L, the usual order of magnitude<br />

generally implies ε = EI<br />

TL2 ≪ 1sothat(22.173)<br />

can be written:<br />

ω 2 = k 2 c 2� 1 + εk 2 L 2� . (22.174)<br />

For a stiff string with hinged ends the boundary<br />

conditions impose<br />

sin kL = 0 sothat kn L = nπ (22.175)

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