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11 #X text 483 512 Calculates the frequency;
|
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|
12 #X text 484 524 based on the physics of;
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13 #X text 107 382 Calculates the gain of the dipole source;
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|
14 #X text 469 47 Azimuth;
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15 #X text 651 49 Pan;
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16 #X text 543 51 Elevation;
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17 #X text 394 52 Distance;
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r@194
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86 #X text 273 27 Generates the sound associated with the lift dipole.
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|
87 ;
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|
88 #X text 318 326 Generates the sound associated with the drag dipole.
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89 ;
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246 #X text 533 2 Distance;
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247 #X text 724 595 Calculates Drag Dipole gain;
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248 #X text 48 508 Calculates Lift Dipole gain;
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259 #X text 268 112 Wind speed;
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310 #X text 709 1 Azimuth;
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311 #X text 608 3 Elevation;
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312 #X text 892 379 Speed of Sound to power 3;
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313 #X obj 872 423 /~;
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314 #X text 588 167 Remember - Goldstein moves cylinder;
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315 #X obj 518 170 /~ 360;
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316 #X obj 758 475 *~;
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317 #X obj 218 205 *~;
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318 #X obj 234 417 sin~;
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319 #X obj 404 167 *~;
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r@194
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320 #X obj 404 141 r~ \$0-thisDist;
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r@194
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321 #X obj 520 40 s~ \$0-thisDist;
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322 #X obj 513 18 inlet~;
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323 #X obj 404 220 *~ 32;
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324 #X obj 404 193 *~ 4.05513e+07;
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325 #X obj 713 19 inlet~;
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326 #X obj 720 44 s~ \$0-gain_azim;
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327 #X obj 283 392 r~ \$0-gain_azim;
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328 #X obj 611 21 inlet~;
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329 #X obj 887 312 r~ \$0-thisDist;
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330 #X obj 887 336 *~;
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331 #X obj 887 361 *~ 4.05513e+07;
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332 #X obj 887 399 *~ 32;
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333 #X obj 616 44 s~ \$0-gain_elev;
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334 #X obj 518 130 r~ \$0-gain_elev;
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335 #X obj 723 315 r~ \$0-gain_elev;
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336 #X obj 234 369 r~ \$0-gain_elev;
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337 #X obj 240 258 r bladeLen;
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338 #X text 25 173 St ^2 * mass air * sqrt(2*pi);
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339 #X obj 218 171 *~ 0.1228;
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340 #X obj 293 192 *~ 5;
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341 #X obj 293 170 sig~;
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342 #X obj 551 191 /~ 343.56;
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343 #X obj 773 336 r~ \$0-gain_azim;
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406 #X restore 127 322 pd GoldfreqGainLoFi;
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431 #X connect 45 0 19 0;
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432 #X connect 45 1 18 0;
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r@194
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433 #X connect 46 0 1 0;
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