comparison AeolianHarp/stringE.pd @ 104:078bc293e072

Aeolian harp file updated

+#N canvas -9 64 1440 700 10;
+#X text 818 -13 Mass Density of Air;
+#X text 127 302 Frequency (Hz);
+#X obj 895 435 throw~ l;
+#X obj 922 416 throw~ r;
+#X obj 910 289 osc~;
+#X obj 940 -12 *~ 1.225;
+#X obj 940 63 /~ 1.81e-05;
+#X obj 940 18 *~ 1;
+#X obj 910 238 /~ 1;
+#X floatatom 221 282 10 0 0 0 - - -;
+#X obj 925 106 /~;
+#X obj 910 214 *~;
+#X obj 910 263 clip~ 0 20000;
+#X obj 232 -71 inlet;
+#X text 781 56 Reynolds Number;
+#X text 794 230 Strouhal Number;
+#X obj 393 -73 inlet;
+#X obj 910 319 *~;
+#X text 970 43 Viscosity;
+#X obj 674 240 *~ 2;
+#X obj 674 267 osc~;
+#X obj 674 289 *~;
+#X obj 895 348 +~;
+#X obj 232 -47 s \$0-diameter;
+#X obj 1001 -13 r \$0-diameter;
+#X obj 990 187 r \$0-diameter;
+#X obj 149 -9 s~ \$0-windSpeed;
+#X obj 338 60 r~ \$0-windSpeed;
+#X obj 989 156 r~ \$0-windSpeed;
+#X obj 940 -40 r~ \$0-windSpeed;
+#X obj 845 213 s~ \$0_str;
+#X obj 328 39 r~ \$0_str;
+#X obj 707 267 r~ \$0_dragDiGain;
+#X obj 825 289 s~ \$0-myFreq;
+#X obj 674 219 r~ \$0-myFreq;
+#X obj 948 289 r~ \$0_liftDiGain;
+#X obj 149 -51 sig~;
+#X obj 149 -30 vd~ varwind;
+#X obj 149 -75 inlet;
+#X obj 1161 19 r~ \$0-myFreq;
+#X obj 1127 -31 noise~;
+#X obj 1204 203 throw~ l;
+#X obj 1231 182 throw~ r;
+#X obj 1204 110 *~;
+#X obj 143 104 snapshot~;
+#X obj 143 79 metro 100;
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+1;
+#X floatatom 143 130 10 0 0 0 - - -;
+#X obj 143 31 loadbang;
+#X obj 69 79 r~ \$0-myRey;
+#X obj 953 87 s~ \$0-myRey;
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+#X obj 1342 -53 loadbang;
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+1 1;
+#X obj 1253 -82 r~ \$0-myRey;
+#X obj 1169 371 r~ \$0-myFreq;
+#X obj 1135 300 noise~;
+#X obj 1212 560 throw~ l;
+#X obj 1239 537 throw~ r;
+#X obj 1212 468 *~;
+#X obj 1350 380 snapshot~;
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+#X obj 1350 332 tgl 15 0 empty empty empty 17 7 0 10 -262144 -1 -1
+1 1;
+#X obj 1261 278 r~ \$0-myRey;
+#X obj 1169 397 *~ 2;
+#X text 128 150 Reynolds Number;
+#X obj 1127 62 vcf~ 1000 10;
+#X obj 1135 422 vcf~ 1000 10;
+#X obj 895 391 fcpan;
+#X obj 1204 159 fcpan;
+#X obj 1212 512 fcpan;
+#X obj 1219 83 *~ 1;
+#X obj 1227 443 *~ 1;
+#X obj 1261 353 clip~ 2 400;
+#X obj 1253 -7 clip~ 2 400;
+#X obj 1261 302 *~ -0.003;
+#X obj 1253 -58 *~ -0.003;
+#X obj 1342 -5 metro 10;
+#X obj 1350 355 metro 10;
+#X obj 393 -53 s \$0_dist;
+#X obj 626 -80 inlet;
+#X obj 626 -11 s \$0_thisPan;
+#X obj 922 362 r \$0_thisPan;
+#X obj 1231 135 r \$0_thisPan;
+#X obj 1239 490 r \$0_thisPan;
+#X floatatom 571 -11 8 0 0 0 - - -;
+#X obj 626 -56 max 0.1;
+#X obj 626 -33 min 0.9;
+#X text 1263 456 Drag Dipole spectrum calculation;
+#X text 1258 100 Lift Dipole spectrum calculation;
+#X text 661 102 Calculates the frequency;
+#X text 661 115 based on the physics of;
+#X text 662 128 the object and environment;
+#X obj 335 319 r~ \$0-windSpeed;
+#X obj 324 296 r~ \$0_str;
+#X obj 1227 420 r~ \$0_dragNoiseGain;
+#X obj 1219 41 r~ \$0_liftNoiseGain;
+#X obj 891 67 sig~ 1;
+#X obj 925 132 sqrt~;
+#X obj 925 157 *~ 1.0356;
+#X obj 851 148 sig~ 0.2684;
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+#X text -21205 129 Mass Density of Air \, squared;
+#X text -20857 164 Speed of Sound to power 2;
+#X obj -21070 29 *~;
+#X obj -21022 70 *~;
+#X obj -21022 104 *~ 1;
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+#X obj -20859 141 * 118033;
+#X obj -21022 193 /~ 1;
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+#X text -20859 71 Distance;
+#X obj -20890 352 cos;
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+#X text -20895 510 Calculates Drag Dipole gain;
+#X text -21175 486 Calculates Lift Dipole gain;
+#N canvas 759 125 286 289 pow8 0;
+#X obj 47 67 *~;
+#X obj 76 67 *~;
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+#X text -20947 211 Azimuth;
+#X text -20871 210 Elevation;
+#X text -20961 26 Gain proportional to windspeed to power 8 for spectrum
+;
+#X text -20981 74 Diameter;
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+#X text 287 77 Elevation Angle;
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+#X obj 278 360 /;
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+#X obj 278 414 * 2;
+#X text 318 296 Arccos of angle;
+#X obj 293 236 + 1;
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+#X text 56 42 Azimuth Angle;
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+#X restore -20942 252 pd angleCalc;
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+#X obj -21000 305 / 360;
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+#X obj -21021 397 *~ 1;
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+#X text -20848 459 Need for scienctific reasoning here!;
+#X text -21239 441 Need for scienctific reasoning here!;
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+#X text 36 127 Mass Density of Air \, squared;
+#X text 508 93 Speed of Sound to power 2;
+#N canvas 759 125 286 289 pow6 0;
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+#X text 497 1 Distance;
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+#X text 476 498 Calculates Drag Dipole gain;
+#X text 48 445 Calculates Lift Dipole gain;
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+#X text 132 473 Strouhal Number;
+#X text 318 251 Calculates the gain of the dipole source;
+#X text 315 512 Calculates the gain of the source;
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+#X connect 138 0 133 0;
+#X connect 140 0 132 1;
+#X connect 141 0 142 0;
+#X connect 142 0 137 1;
+#X connect 152 0 153 0;
+#X connect 152 0 155 0;
+#X connect 156 0 110 3;
+#X connect 157 0 117 3;
+#X connect 158 0 76 0;
+#X connect 159 0 75 0;