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5 #X obj 240 96 s \$0-diameter;
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r@216
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9 #X obj 519 493 s~ \$0-myFreq;
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10 #X obj 646 67 inlet;
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11 #X text 483 512 Calculates the frequency;
|
|
r@216
|
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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18 #X text 228 52 Diameter;
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19 #X text 143 51 Wind Speed;
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r@216
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r@216
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r@216
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r@216
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r@216
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46 #X obj 621 86 *~ 5;
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47 #X obj 353 93 *~ 3;
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r@216
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48 #X obj 215 359 r~ \$0-myFreq;
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r@216
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49 #X obj 230 432 r~ \$0-dragDiGain;
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r@216
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51 #X obj 494 358 r~ \$0-myFreq;
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r@216
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r@216
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r@216
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56 #X obj 210 264 throw~ l;
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57 #X obj 237 241 throw~ r;
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r@216
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58 #X obj 210 220 fcpan;
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r@216
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59 #X obj 237 198 r \$0-thisPan;
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r@216
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60 #X obj 210 67 r~ \$0-thisNoise;
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r@216
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61 #X obj 480 192 *~;
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r@216
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62 #X obj 480 257 throw~ l;
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63 #X obj 507 234 throw~ r;
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r@216
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64 #X obj 480 213 fcpan;
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r@216
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r@216
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66 #X obj 480 68 r~ \$0-thisNoise;
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67 #X obj 750 183 *~;
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68 #X obj 750 248 throw~ l;
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69 #X obj 777 225 throw~ r;
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r@216
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70 #X obj 750 204 fcpan;
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r@216
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71 #X obj 777 182 r \$0-thisPan;
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r@216
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72 #X obj 750 65 r~ \$0-thisNoise;
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73 #X obj 636 147 *~ 0.1;
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74 #X obj 360 478 *~;
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r@216
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76 #X obj 387 520 throw~ r;
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r@216
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77 #X obj 360 499 fcpan;
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r@216
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78 #X obj 387 477 r \$0-thisPan;
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r@216
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r@216
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85 #X obj 634 358 r~ \$0-thisNoise;
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r@216
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86 #X text 273 27 Generates the sound associated with the lift dipole.
|
|
r@216
|
87 ;
|
|
r@216
|
88 #X text 318 326 Generates the sound associated with the drag dipole.
|
|
r@216
|
89 ;
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r@216
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r@216
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170 #X restore 774 538 pd Dipoles;
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181 #N canvas 181 90 1238 721 GoldfreqGainLoFi 1;
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182 #N canvas 759 125 286 294 pow6 0;
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245 #X restore 218 145 pd pow6;
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r@216
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246 #X text 533 2 Distance;
|
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r@216
|
247 #X text 724 595 Calculates Drag Dipole gain;
|
|
r@216
|
248 #X text 48 508 Calculates Lift Dipole gain;
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r@216
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249 #X obj 218 112 inlet~;
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258 #X obj 219 463 *~;
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259 #X text 268 112 Wind speed;
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260 #X text 321 196 Corr Length;
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263 #X obj 283 437 cos~;
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265 #X text 370 104 Speed of Sound to power 3;
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r@216
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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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320 #X obj 404 141 r~ \$0-thisDist;
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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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363 #X connect 26 0 27 1;
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364 #X connect 27 0 13 0;
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405 #X connect 72 0 35 0;
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406 #X restore 127 322 pd GoldfreqGainLoFi;
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407 #X obj 519 387 sig~ 0.2;
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r@216
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r@216
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416 #X connect 22 0 45 1;
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417 #X connect 23 0 24 0;
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r@216
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r@216
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r@216
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r@216
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r@216
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424 #X connect 33 0 34 0;
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r@216
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425 #X connect 35 0 45 3;
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r@216
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426 #X connect 37 0 38 0;
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r@216
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427 #X connect 38 0 39 0;
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r@216
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428 #X connect 40 0 41 0;
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r@216
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429 #X connect 42 0 44 0;
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r@216
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430 #X connect 44 0 43 0;
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r@216
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431 #X connect 45 0 19 0;
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r@216
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432 #X connect 45 1 18 0;
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r@216
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433 #X connect 46 0 1 0;
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