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r@274: #X text 28 383 Calculates the frequency;
r@274: #X text 29 395 based on the physics of;
r@274: #X text 292 401 Calculates the gain of the dipole source;
r@274: #X text 419 318 Azimuth;
r@274: #X text 383 247 Elevation;
r@274: #X text 366 216 Distance;
r@274: #X text 330 156 Diameter;
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r@267: #X text 101 35 Generates the sound associated with the lift dipole.
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r@274: #X text 29 408 the object and environment;
r@274: #X text 291 110 Source Speed;
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r@267: #X text 587 13 Distance;
r@267: #X text 48 531 Calculates Lift Dipole gain;
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r@267: #X text 74 100 Strouhal number;
r@267: #X text 216 46 Wind speed;
r@267: #X text 281 146 Corr Length;
r@267: #X text -86 235 Mass Density of Air;
r@267: #X text 108 242 Sqrt(2xpi);
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r@267: #X text 763 12 Azimuth;
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r@267: #X text 512 235 Remember - Goldstein moves cylinder;
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r@267: #X text -214 358 If adding additional signal at 0 degrees then you
r@267: will have to add it before you divid by distance - for all sources!
r@267: ;
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r@267: #X text -154 219 Scale factor to bring in line with CFD calcs (divided
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r@269: #X text -84 298 First section of the Reynolds number - DeltaF/F relationship
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r@269: #X text 565 329 Third section of the Reynolds number - DeltaF/F relationship
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