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Analysis and Ranking of the Acoustic Disturbance Potential of ...

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FIG. 4.1 CORRECTION TO 300 M REFERENCE SPECTRA FOR AIRCRAFT FLYOVER AT $<br />

OTHER ALTITUDES (St<strong>and</strong>ard Day conditions)<br />

cr q<br />

1 . 1 .<br />

P<br />

.<br />

z<br />

0<br />

Q\<br />

a<br />

Cr<br />

V1<br />

I * .<br />

I ' .<br />

m<br />

0<br />

0--<br />

C<br />

m<br />

-I=<br />

I 0<br />

m<br />

& F z<br />

c 8 V1<br />

0 -lo-- -e 1 km<br />

L<br />

0<br />

0 -20--<br />

L<br />

1<br />

C3<br />

8 '?<br />

* 20 40 80 160 315 630 1250 2500 5000 10000 %<br />

p<br />

1/3 Octave B<strong>and</strong> Center Frequency<br />

I<br />

a<br />

2<br />

0<br />

i?<br />

T.<br />

(D<br />

cn

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