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Flute acoustics: measurement, modelling and design - School of ...

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20 CHAPTER 2. THEORY AND LITERATURE REVIEW<br />

<br />

<br />

Figure 2.4: The acoustic reactance X <strong>and</strong> the acoustic resistance R as functions <strong>of</strong> ka for an<br />

infinitely flanged pipe (a) <strong>and</strong> an unflanged pipe (b). X <strong>and</strong> R are both in units <strong>of</strong> ρc/πa 2<br />

(Fletcher & Rossing 1998, after Beranek (1954)).<br />

The impedance (including radiation loss) <strong>of</strong> an unflanged pipe was calculated by Levine &<br />

Schwinger (1948). Dalmont et al. (2001) give simple fit formulae for the frequency-dependent<br />

end correction <strong>and</strong> the magnitude <strong>of</strong> the reflection coefficient:<br />

[ 1 + 0.044(ka)<br />

2<br />

]<br />

˜δ open = δ open<br />

1 + 0.19(ka) 2 − 0.02sin2 (2ka) for ka < 1.5 (2.21)<br />

<strong>and</strong><br />

1 + 0.2ka− 0.084(ka) 2<br />

|R open |=<br />

1 + 0.2ka+ ( 1 for ka < 3.5. (2.22)<br />

2<br />

− 0.084)(ka)2<br />

2.2.8.2 Infinitely flanged pipe<br />

The low-frequency, lossless end correction for an infinitely flanged pipe is greater than for<br />

a unflanged pipe, since the solid angle for radiation is reduced (Dalmont et al. 2001):<br />

δ flanged = 0.8216a. (2.23)<br />

Rayleigh (1894) <strong>and</strong> Nomura et al. (1960) give the impedance for an infinitely flanged pipe. Fit<br />

formulae by Norris & Sheng (1989) are accurate for ka < 3.5:<br />

[<br />

] −1<br />

˜δ flanged = δ flanged 1 + (0.77ka)2<br />

(2.24)<br />

1 + 0.77ka<br />

<strong>and</strong><br />

|R flanged |=<br />

1 + 0.323ka− 0.077(ka)2<br />

1 + 0.323ka+ (1 − 0.077)(ka) 2 . (2.25)

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