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Getting to Grips with Aircraft Noise

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Flight Operations Support & Line Assistance<br />

<strong>Getting</strong> <strong>to</strong> grips <strong>with</strong> aircraft noise<br />

9 - A BIT OF THEORY<br />

9.3.3. ADDING SOUND PRESSURE LEVELS – NOTION OF MASKING<br />

EFFECT<br />

In the case of several independent sound sources, it is not possible <strong>to</strong> add arithmetically<br />

the decibel values, as they are logarithmically defined.<br />

Let us consider two sound sources, each of them emitting a pure <strong>to</strong>ne at different<br />

frequencies ω1 and ω2 (corresponding characteristic periods are T1 and T2)<br />

Source 1: ω 1<br />

The resulting sound pressure at a given point is then:<br />

p ( t)<br />

= p1(<br />

t)<br />

+ p2<br />

( t)<br />

(9.3.3-1)<br />

p1max<br />

p2<br />

max<br />

p ( t)<br />

= cos(<br />

ωωωω 1(<br />

t − r1<br />

/ c)<br />

) + cos(<br />

ωωωω 2 ( t − r2<br />

/ c)<br />

)<br />

r<br />

r<br />

(9.3.3-2)<br />

1<br />

The corresponding effective sound pressure is (considering a period T that is the lowest<br />

common multiple of T1 and T2:<br />

p<br />

r 1<br />

2<br />

e<br />

r 2<br />

Source 2: ω 2<br />

2<br />

T<br />

1 ⎡ p1max<br />

p2<br />

max<br />

⎤<br />

= ∫ ⎢⎣<br />

cos(<br />

ωωωω 1 ( t − r1<br />

/ c)<br />

) + cos(<br />

ωωωω 2 ( t − r2<br />

/ c)<br />

) ⎥ dt<br />

T r<br />

r<br />

0 1<br />

2<br />

⎦<br />

(9.3.3-3)<br />

2<br />

63

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