diff MechAeolianD3.pd @ 0:12b68fb81455

Demo patch for Aeolian Harp synthesis model
author Rod Selfridge <r.selfridge@qmul.ac.uk>
date Wed, 23 Nov 2016 12:24:24 +0000
parents
children 432a4398d556
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line diff
--- /dev/null	Thu Jan 01 00:00:00 1970 +0000
+++ b/MechAeolianD3.pd	Wed Nov 23 12:24:24 2016 +0000
@@ -0,0 +1,1977 @@
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+#X text 234 22 Y = 10^b . X^m;
+#X text 235 40 b = 1.536;
+#X text 235 56 m = -0.245;
+#X text 51 364 Equation of line derived from Norberg 2001;
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+#X text 273 27 Generates the sound associated with the lift dipole.
+;
+#X text 312 370 Generates the sound associated with the drag dipole.
+;
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+#X text 60 485 Generate sounds associated with the Aeolian tone. Higher
+harmonics have been removed compares to AES paper. This is because
+they have such a small contribution in comparison to lower harmonics
+and the FM spectrum during lock-in;
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+#X obj 618 261 + 16.5;
+#X obj 618 238 +;
+#X text -84 298 First section of the Reynolds number - DeltaF/F relationship
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+#X text 565 329 Third section of the Reynolds number - DeltaF/F relationship
+is linear and did not appear to be reliant on current TU values;
+#X text 114 -16 Middle section of Reynolds number - DeltaF/F relationship
+is also linear but depends on TU Value;
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+#X text 74 717 Patch that calcultes the natural or fundamental frequency
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+the linear mass density.;
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+#X text 161 252 Strouhal No;
+#X text 281 235 Reynolds No;
+#X obj 101 23 *~ 67679.6;
+#X text 210 22 Cosolidation of 2pi \, air density and viscosity in
+equations identified in original AES paper - Aeolian tone.;
+#X text 43 252 Strouhal Frequency;
+#X obj 101 94 clip~ 40 1e+06;
+#X text 210 109 Reynolds number clipped at lower limit of 40 to prevent
+Strouhal number decreasing to negative numbers - due to relationship
+identified in Fey paper.;
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+#X text 100 346 Calculates the modulation frequency from the difference
+between the shedding and natural frequency - Van Atta paper.;
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+#X text 361 199 f(s)[n]+β(f(eta)[n]−f(s)[n]);
+#X text 655 204 f(s)[n]-β(f(s)[n]−f(eta)[n]);
+#X text 36 291 Calculates the value of β from the Red Velocity V;
+#X text 229 371 Patch that calculates the vortex shedding frequency
+from the values of the Strouhal Frequency \, Harmonic of the natural
+vibration frequency and the reduced velocity.;
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+#X text 37 89 V = u/(2pi.f.d);
+#X text 254 149 Harmonic Number;
+#X msg 217 168 \$1 40;
+#X text 38 373 Patch that calculates the Reduced Velocity \, V.;
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+#X obj 72 644 outlet~;
+#N canvas 0 27 450 362 PlotWrt 0;
+#X obj 116 303 textfile;
+#X msg 330 202 clear \, rewind;
+#X msg 169 202 add \$1;
+#X msg 116 202 add2 \$1;
+#X obj 105 92 snapshot~;
+#X floatatom 119 129 0 0 0 0 - - -;
+#X obj 198 92 snapshot~;
+#X floatatom 250 119 0 0 0 0 - - -;
+#X obj 25 15 inlet~;
+#X obj 343 45 inlet~;
+#X obj 105 67 r myMet;
+#X obj 198 67 r myMet;
+#X msg 218 202 write hystTest2.txt;
+#X connect 1 0 0 0;
+#X connect 2 0 0 0;
+#X connect 3 0 0 0;
+#X connect 4 0 5 0;
+#X connect 4 0 3 0;
+#X connect 6 0 7 0;
+#X connect 6 0 2 0;
+#X connect 8 0 4 0;
+#X connect 9 0 6 0;
+#X connect 10 0 4 0;
+#X connect 11 0 6 0;
+#X connect 12 0 0 0;
+#X restore -6 583 pd PlotWrt;
+#X floatatom 103 460 0 0 0 0 - - -;
+#X floatatom 58 461 0 0 0 0 - - -;
+#N canvas 432 91 476 532 Hyst1 0;
+#X obj 184 20 inlet~;
+#X obj 309 66 snapshot~;
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+#X floatatom 356 91 0 0 0 0 - - -;
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+#X floatatom 270 136 0 0 0 0 - - -;
+#X obj 184 69 snapshot~;
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+#X floatatom 102 93 0 0 0 0 - - -;
+#X obj 184 46 delta~;
+#X obj 184 92 > 0;
+#X obj 235 91 < 0;
+#X obj 234 267 - 1;
+#X obj 234 287 * -1;
+#X floatatom 291 310 0 0 0 0 - - -;
+#N canvas 582 482 491 257 accDec 0;
+#X obj 91 77 r myMet;
+#X obj 224 20 inlet;
+#X obj 268 21 inlet;
+#X obj 91 98 spigot;
+#X msg 91 119 1;
+#X obj 153 78 r myMet;
+#X obj 153 99 spigot;
+#X msg 153 120 0;
+#X floatatom 91 141 0 0 0 0 - - -;
+#X obj 153 142 outlet;
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+#X obj 298 93 spigot;
+#X msg 298 114 1;
+#X obj 360 73 r myMet;
+#X obj 360 94 spigot;
+#X msg 360 115 0;
+#X obj 360 137 outlet;
+#X floatatom 298 135 0 0 0 0 - - -;
+#X text 88 177 Identifies if the Reduced Velocity is increasing or
+decreasing.;
+#X connect 0 0 3 0;
+#X connect 1 0 6 1;
+#X connect 1 0 11 1;
+#X connect 2 0 3 1;
+#X connect 2 0 14 1;
+#X connect 3 0 4 0;
+#X connect 4 0 8 0;
+#X connect 4 0 9 0;
+#X connect 5 0 6 0;
+#X connect 6 0 7 0;
+#X connect 7 0 8 0;
+#X connect 7 0 9 0;
+#X connect 10 0 11 0;
+#X connect 11 0 12 0;
+#X connect 12 0 16 0;
+#X connect 12 0 17 0;
+#X connect 13 0 14 0;
+#X connect 14 0 15 0;
+#X connect 15 0 16 0;
+#X connect 15 0 17 0;
+#X restore 184 113 pd accDec;
+#X obj 151 166 spigot;
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+#X obj 169 213 spigot;
+#X floatatom 136 282 0 0 0 0 - - -;
+#X obj 168 281 outlet;
+#X obj 234 311 outlet;
+#X obj 202 189 > 1.06;
+#X obj 169 244 < 0.9;
+#X text 52 371 This patch identifies which path of the hysteresis curve
+the reduced velocity is on. It keeps it locked into this path between
+the values of 0.9 and 1.06. Outwith these values both legs are approx
+the same.;
+#X text 67 -14 Goal - If output = 1 at any time then keep it at one
+until other input = 1;
+#X connect 0 0 9 0;
+#X connect 0 0 1 0;
+#X connect 1 0 3 0;
+#X connect 1 0 16 0;
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+#X connect 6 0 8 0;
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+#X connect 7 0 6 0;
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+#X connect 13 0 21 0;
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+#X connect 15 1 5 0;
+#X connect 15 1 17 1;
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+#X connect 18 0 23 0;
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+#X connect 23 0 19 0;
+#X connect 23 0 12 0;
+#X connect 23 0 20 0;
+#X restore 58 439 pd Hyst1;
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+#X obj 11 353 +~;
+#X obj -153 333 -~ 1;
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+#X obj -41 408 +~;
+#X obj 72 495 +~;
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+#X obj 304 313 *~ 50;
+#X obj 814 202 inlet;
+#X obj -35 219 -~ 1.02;
+#X obj -123 220 -~ 0.92;
+#X obj -123 242 *~ 33;
+#X obj -153 353 *~ -1.3;
+#X obj -35 241 *~ 200;
+#X obj 239 248 *~ 33;
+#X msg 566 -22 1.6;
+#X obj 151 248 *~ 200;
+#X msg 520 -24 0.4;
+#X obj 799 112 r \$0-mass;
+#X obj 799 135 / 1.225;
+#X msg 799 158 \$1 20;
+#X obj 799 177 line~;
+#X text 853 139 m* = rho_m / rho_f;
+#X floatatom 874 264 0 0 0 0 - - -;
+#X obj 829 245 t f b;
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+#X obj 814 268 *;
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+#X obj 458 347 *~;
+#X obj 458 303 *~ -1.29;
+#X obj 443 408 *~ 0.63;
+#X obj 443 262 sig~ 1;
+#X obj 443 324 +~;
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+#X obj 443 386 +~;
+#X obj 563 118 r~ \$0-myApl;
+#X obj 563 184 *~;
+#X obj 548 99 sig~ 1;
+#X obj 548 161 +~;
+#X obj 578 161 r~ \$0-myApl;
+#X obj 548 228 +~;
+#X obj 563 140 *~ -1.12;
+#X obj 563 205 *~ 0.3;
+#X obj 458 367 *~ 0.59;
+#X obj 548 356 *~;
+#X obj 72 516 /~ 1.2;
+#X obj 482 458 +~;
+#X obj 239 227 -~ 0.9;
+#X obj 248 138 < 0.86;
+#X obj 151 226 -~ 0.89;
+#X obj -64 142 >= 0.995;
+#X floatatom 925 219 0 0 0 0 - - -;
+#X text 128 643 A/d;
+#X text -198 62 Sigmoid functions replicating the inital branch of
+the hysteresis curve.;
+#X text 151 60 Sigmoid functions replicating the lower branch of the
+hysteresis curve.;
+#X text 681 23 Test objects;
+#X obj -153 374 spigot~;
+#X text -303 477 By time decent kicks in the other sigmoids will be
+= 1 therefore the multiplication of the decending sigmoid rather than
+adding.;
+#X text 855 199 Damping input;
+#X text 864 286 Harmonic number;
+#X text -117 521 Normalises the Hysteresis plot;
+#X obj -171 17 s~ \$0-thisV;
+#X obj -30 80 r~ \$0-thisV;
+#X obj -123 199 r~ \$0-thisV;
+#X obj -35 197 r~ \$0-thisV;
+#X obj 26 266 r~ \$0-thisV;
+#X obj 58 403 r~ \$0-thisV;
+#X obj -6 560 r~ \$0-thisV;
+#X obj 151 203 r~ \$0-thisV;
+#X obj 270 76 r~ \$0-thisV;
+#X obj 238 205 r~ \$0-thisV;
+#X obj 304 269 r~ \$0-thisV;
+#X text 424 241 Low Re route;
+#X text 468 125 High Re route;
+#X text 715 422 Clipped to match the range given in Govardhan paper
+as well as to stop the value exploding after 1.5;
+#X obj 587 409 <= 500;
+#X msg 622 -11 1.6 30000;
+#X msg 695 0 0.4 30000;
+#X obj -171 -5 inlet~;
+#X obj 72 560 clip~ 0 2;
+#X obj 799 352 clip~ 0 1.5;
+#X obj 72 538 *~;
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+#X msg 814 289 \$1 40;
+#X obj 72 581 snapshot~;
+#X obj 164 562 r myMet;
+#X obj 72 622 vline~;
+#X msg 72 601 \$1 50;
+#X text 124 607 Smoothing;
+#X text 234 594 This patch takes the Reduced Velocity V value \, (\$0-thisV)
+and calculates the corresponding value of maximum vibration \, A/d.
+;
+#X text 493 491 Calculates Amax;
+#X connect 0 0 2 0;
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+#X connect 61 0 1 0;
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+#X connect 62 0 120 0;
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+#X connect 64 0 65 0;
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+#X connect 70 0 7 0;
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+#X connect 75 0 94 0;
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+#X connect 85 0 115 1;
+#X connect 86 1 115 0;
+#X connect 87 0 88 0;
+#X connect 88 0 90 0;
+#X connect 89 0 88 1;
+#X connect 90 0 91 0;
+#X connect 91 0 113 1;
+#X connect 92 0 91 1;
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+#X connect 96 0 98 0;
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+#X connect 98 0 101 1;
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+#X connect 100 0 101 0;
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+#X connect 102 0 97 0;
+#X connect 102 0 97 1;
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+#X connect 105 0 111 0;
+#X connect 106 0 107 0;
+#X connect 107 0 109 0;
+#X connect 108 0 105 0;
+#X connect 108 0 105 1;
+#X connect 109 0 113 0;
+#X connect 110 0 107 1;
+#X connect 111 0 109 1;
+#X connect 112 0 103 1;
+#X connect 113 0 85 0;
+#X connect 114 0 150 0;
+#X connect 115 0 150 1;
+#X connect 116 0 68 0;
+#X connect 117 0 11 1;
+#X connect 117 0 47 1;
+#X connect 117 0 55 0;
+#X connect 118 0 70 0;
+#X connect 119 0 35 1;
+#X connect 119 0 125 1;
+#X connect 125 0 36 0;
+#X connect 131 0 13 0;
+#X connect 132 0 64 0;
+#X connect 133 0 63 0;
+#X connect 134 0 57 0;
+#X connect 135 0 19 0;
+#X connect 136 0 16 0;
+#X connect 137 0 118 0;
+#X connect 138 0 45 0;
+#X connect 139 0 116 0;
+#X connect 140 0 56 0;
+#X connect 144 0 85 1;
+#X connect 144 0 86 1;
+#X connect 145 0 41 0;
+#X connect 146 0 41 0;
+#X connect 147 0 130 0;
+#X connect 148 0 16 1;
+#X connect 148 0 154 0;
+#X connect 149 0 95 0;
+#X connect 150 0 148 0;
+#X connect 152 0 78 0;
+#X connect 152 0 77 0;
+#X connect 153 0 93 0;
+#X connect 154 0 157 0;
+#X connect 155 0 154 0;
+#X connect 156 0 15 0;
+#X connect 157 0 156 0;
+#X restore 1161 268 pd SimpHyst;
+#X obj 1161 207 r~ \$0-redVel;
+#X obj 1192 227 r \$0-dampPar;
+#X obj 1224 246 r \$0-harmNo;
+#X obj 1161 288 s~ \$0-AdVal;
+#X obj 1265 484 r~ \$0-AdVal;
+#N canvas 361 196 756 527 FMout 0;
+#X obj 170 -2 inlet~;
+#X obj -67 61 osc~;
+#X obj -67 384 throw~ l;
+#X obj -56 363 throw~ r;
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+#X obj -52 15 inlet~;
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+#X obj -67 37 +~;
+#X obj -48 188 osc~;
+#X obj -67 232 +~;
+#X obj -3 118 r mod;
+#X obj -48 95 inlet~;
+#X obj -33 118 osc~;
+#X obj -33 142 *~ 1;
+#X obj -48 164 +~;
+#X text -40 31 Modulation frequency;
+#X text 81 -24 A/d - max vibration;
+#X text -46 80 Difference frequency;
+#X obj 170 20 s~ \$0-myAd;
+#X obj -52 251 r~ \$0-myAd;
+#X text -191 -32 Fv \, vortex shedding freq;
+#X obj 1 320 inlet;
+#X text 35 322 on/off;
+#X obj -67 321 *~ 5e-05;
+#X obj -67 273 *~;
+#X text -329 265 Vibration value as calculated in SimpHyst;
+#X text -399 56 High Frequency FM Spectrum around the vortex shedding
+frequency;
+#X text -405 204 Low Frequency spectrum around the difference frequency
+;
+#X text -432 328 Gain value to strike a balance between the FM spectrums
+and the output from the dipoles due to the Aeolian Tone;
+#X text -235 449 Patch that calculates the full FM spectrum and scales
+it according to the vibration amount A as well as a ratio to the Aeolian
+tone dipoles.;
+#X text 6 376 Send signal to the DAC;
+#X text 11 203 LF Spectrum is at lower level that HF one;
+#X obj -48 208 *~ 0.1;
+#X obj -67 300 *~;
+#X obj -36 274 r~ \$0-reyGain;
+#X connect 0 0 18 0;
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+#X connect 10 0 13 1;
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+#X connect 11 0 12 0;
+#X connect 12 0 13 0;
+#X connect 13 0 14 1;
+#X connect 14 0 8 0;
+#X connect 19 0 24 1;
+#X connect 21 0 6 1;
+#X connect 23 0 6 0;
+#X connect 24 0 33 0;
+#X connect 32 0 9 1;
+#X connect 33 0 23 0;
+#X connect 34 0 33 1;
+#X restore 1221 504 pd FMout;
+#X obj 727 526 s~ \$0-vorFreq;
+#X obj 474 647 r~ \$0-vorFreq;
+#X obj 1221 401 r~ \$0-vorFreq;
+#X obj 1039 419 r~ \$0-vorFreq;
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+#X text 773 299 Calcs Harmonic No;
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