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1 #N canvas 65 37 1227 739 10;
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r@214
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2 #X text 597 188 Mass Density of Air;
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r@214
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3 #X obj 719 189 *~ 1.225;
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r@214
|
4 #X obj 719 264 /~ 1.81e-05;
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r@214
|
5 #X obj 719 219 *~ 1;
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|
r@214
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6 #X obj 719 358 *~;
|
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r@214
|
7 #X text 752 308 Reynolds Number;
|
|
r@214
|
8 #X text 599 375 Strouhal Number;
|
|
r@214
|
9 #X text 749 244 Viscosity;
|
|
r@214
|
10 #X obj 780 188 r \$0-diameter;
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|
11 #X obj 719 451 s~ \$0-myFreq;
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12 #X obj 1062 344 *~;
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14 #X obj 646 67 inlet;
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15 #X floatatom 591 136 8 0 0 0 - - -;
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16 #X text 683 470 Calculates the frequency;
|
|
r@214
|
17 #X text 684 482 based on the physics of;
|
|
r@251
|
18 #X text 307 437 Calculates the gain of the dipole source;
|
|
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|
19 #X text 559 36 Azimuth;
|
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|
20 #X text 651 49 Pan;
|
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|
21 #X text 404 41 Elevation;
|
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r@251
|
22 #X text 284 5 Distance;
|
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r@214
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23 #X text 228 52 Diameter;
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r@214
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r@214
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r@251
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r@251
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29 #X obj 336 464 r~ \$0-str;
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r@250
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31 #X obj 619 360 s~ \$0-str;
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32 #X obj 646 136 s \$0-thisPan;
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34 #X obj 1089 344 r \$0-thisPan;
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35 #X text 1043 174 Noise spectrum calculation;
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36 #X obj 1077 292 hip~;
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37 #X obj 1077 247 rpole~ 0.99;
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38 #X obj 354 181 r~ \$0-str;
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r@250
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39 #X text 327 700 Calculates the gain of the wake;
|
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|
40 #N canvas 1021 287 444 428 corrLen 0;
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44 #X obj 124 93 sig~ -0.245;
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45 #X obj 103 119 pow~;
|
|
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|
46 #X text 234 22 Y = 10^b . X^m;
|
|
r@214
|
47 #X text 235 40 b = 1.536;
|
|
r@214
|
48 #X text 235 56 m = -0.245;
|
|
r@214
|
49 #X text 80 297 Equation of line derived from Norberg 2001;
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|
50 #X obj 88 169 max~ 1;
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51 #X obj 88 46 sig~ 44.67;
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58 #X restore 718 71 pd corrLen Calc;
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59 #X obj 718 48 r~ \$0-myRey;
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60 #X obj 718 95 s~ \$0-myCor;
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r@251
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61 #X obj 403 271 r~ \$0-myCor;
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62 #X obj 1077 319 hip~;
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63 #X obj 362 508 r~ \$0-myCor;
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r@214
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65 #X obj 646 114 min 0.99;
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66 #N canvas 93 119 976 679 Dipoles 0;
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68 #X obj 225 178 r~ \$0-liftDiGain;
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69 #X obj 389 58 r~ \$0-myFreq;
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70 #X obj 389 82 *~ 3;
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71 #X obj 258 385 r~ \$0-myFreq;
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r@214
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72 #X obj 371 472 r~ \$0-dragDiGain;
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r@214
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73 #X obj 258 407 *~ 2;
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74 #X obj 210 199 *~;
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75 #X obj 210 264 throw~ l;
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r@214
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76 #X obj 237 241 throw~ r;
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r@214
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77 #X obj 210 220 fcpan;
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r@214
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78 #X obj 210 108 vcf~ 3;
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r@214
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79 #X obj 237 198 r \$0-thisPan;
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r@214
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80 #X obj 210 67 r~ \$0-thisNoise;
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r@214
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81 #X obj 480 192 *~;
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r@214
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82 #X obj 480 257 throw~ l;
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r@214
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83 #X obj 507 234 throw~ r;
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r@214
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84 #X obj 480 213 fcpan;
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r@214
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85 #X obj 480 116 vcf~ 3;
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r@214
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86 #X obj 507 191 r \$0-thisPan;
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r@214
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87 #X obj 480 68 r~ \$0-thisNoise;
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r@214
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88 #X obj 338 505 *~;
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r@214
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89 #X obj 338 570 throw~ l;
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r@214
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90 #X obj 365 547 throw~ r;
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r@214
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91 #X obj 338 526 fcpan;
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r@214
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92 #X obj 338 429 vcf~ 3;
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r@214
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93 #X obj 365 504 r \$0-thisPan;
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|
r@214
|
94 #X obj 338 385 r~ \$0-thisNoise;
|
|
r@214
|
95 #X text 273 27 Generates the sound associated with the lift dipole.
|
|
r@214
|
96 ;
|
|
r@214
|
97 #X text 296 353 Generates the sound associated with the drag dipole.
|
|
r@214
|
98 ;
|
|
r@214
|
99 #X obj 270 87 r \$0-Qval;
|
|
r@214
|
100 #X obj 530 92 r \$0-Qval;
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101 #X obj 383 407 r \$0-Qval;
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102 #X floatatom 277 122 5 0 0 0 - - -;
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104 #X obj 480 137 vcf~ 3;
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r@214
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105 #X obj 338 450 vcf~ 3;
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r@244
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106 #X obj 96 232 r myMet;
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109 #X obj 210 158 *~;
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110 #X obj 332 143 r~ broBoost;
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r@244
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111 #X obj 536 114 r~ broBoost;
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112 #X obj 480 159 *~;
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r@244
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113 #X obj 338 472 *~;
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r@244
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114 #X obj 385 447 r~ broBoost;
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r@251
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115 #X obj 727 125 r~ \$0-liftDiGain;
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r@251
|
116 #X obj 706 224 pow~;
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r@251
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117 #X obj 706 104 sig~ 10;
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r@251
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118 #X obj 727 147 /~ 2e-05;
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r@251
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119 #X obj 706 247 *~ 2e-05;
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120 #X obj 727 197 *~ 0.6;
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121 #X obj 801 220 r myMet;
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182 #X connect 56 0 55 1;
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183 #X restore 659 559 pd Dipoles;
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184 #X obj 823 47 noise~;
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185 #X obj 823 70 s~ \$0-thisNoise;
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186 #X obj 1077 224 r~ \$0-thisNoise;
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r@214
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187 #X text 684 495 the object and environment;
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188 #N canvas 308 58 1027 635 StBandwidth 0;
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190 #X obj 460 391 /;
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191 #X obj 460 342 / 100;
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192 #X obj 461 434 outlet;
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193 #X text 437 453 Q value;
|
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|
194 #X obj 531 -36 r~ \$0-myRey;
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195 #X obj 477 -36 r myMet;
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196 #X obj 477 -14 snapshot~;
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198 #X obj 219 187 spigot;
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199 #X obj 236 140 > 0;
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200 #X obj 219 233 + 0.9797;
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r@214
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201 #X obj 219 208 * 4.624e-05;
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202 #X obj 602 150 spigot;
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203 #X obj 618 173 spigot;
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204 #X obj 651 149 < 1e+06;
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205 #X obj 618 216 * 1.227e-10;
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206 #X obj 618 196 *;
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r@214
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207 #X obj 690 215 * -8.553e-05;
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r@214
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208 #X obj 618 261 + 16.5;
|
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|
209 #X obj 618 238 +;
|
|
r@214
|
210 #X text -84 298 First section of the Reynolds number - DeltaF/F relationship
|
|
r@214
|
211 is linear and did not appear to be reliant on current TU values;
|
|
r@214
|
212 #X text 565 329 Third section of the Reynolds number - DeltaF/F relationship
|
|
r@214
|
213 is linear and did not appear to be reliant on current TU values;
|
|
r@214
|
214 #X text 114 -16 Middle section of Reynolds number - DeltaF/F relationship
|
|
r@214
|
215 is also linear but depends on TU Value;
|
|
r@214
|
216 #X obj 461 412 max 0.005;
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r@214
|
217 #X obj 635 126 > 193260;
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253 #X connect 26 0 9 1;
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254 #X connect 29 0 2 0;
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r@214
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255 #X restore 924 69 pd StBandwidth;
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256 #X obj 924 92 s \$0-Qval;
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257 #X obj 1163 267 r myMet;
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259 #X obj 1153 247 r~ \$0-myFreq;
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|
260 #X text 140 51 Source Speed;
|
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r@251
|
261 #X obj 288 24 inlet~;
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r@251
|
262 #X obj 411 62 inlet~;
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r@251
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263 #X obj 563 55 inlet~;
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264 #X obj 288 45 s~ \$0-dist;
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r@214
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265 #X obj 127 75 inlet~;
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r@214
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266 #X obj 59 98 /~ 343.56;
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r@214
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267 #X obj 59 121 s~ \$0-MY_MACH;
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r@251
|
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r@251
|
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|
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r@214
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271 #X obj 429 612 r~ \$0-elev;
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272 #X obj 415 593 r~ \$0-azim;
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|
273 #X obj 402 572 r~ \$0-dist;
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r@214
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275 #X obj 127 95 s~ \$0-sourceSpeed;
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r@214
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276 #X obj 719 161 r~ \$0-sourceSpeed;
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r@214
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277 #X obj 349 486 r~ \$0-sourceSpeed;
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279 #N canvas 51 317 823 563 doppler 0;
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283 #X obj 110 95 r~ \$0-sourceSpeed;
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284 #X obj 125 163 cos~;
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285 #X obj 110 184 *~;
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286 #X obj 286 114 atan;
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|
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291 #X msg 286 161 \$1 15;
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306 current azimuth is the same as the observer azimuth.;
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510 #X text -214 358 If adding additional signal at 0 degrees then you
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r@250
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511 will have to add it before you divid by distance - for all sources!
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512 ;
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r@244
|
923 #X connect 62 0 63 0;
|
|
r@244
|
924 #X connect 64 0 78 5;
|
|
r@244
|
925 #X connect 65 0 78 6;
|
|
r@244
|
926 #X connect 66 0 78 7;
|
|
r@275
|
927 #X connect 66 0 100 0;
|
|
r@244
|
928 #X connect 67 0 79 7;
|
|
r@244
|
929 #X connect 68 0 79 6;
|
|
r@244
|
930 #X connect 69 0 79 5;
|
|
r@244
|
931 #X connect 70 0 78 1;
|
|
r@244
|
932 #X connect 72 0 1 0;
|
|
r@244
|
933 #X connect 73 0 79 1;
|
|
r@244
|
934 #X connect 74 0 4 1;
|
|
r@244
|
935 #X connect 78 0 26 0;
|
|
r@244
|
936 #X connect 78 1 25 0;
|
|
r@244
|
937 #X connect 79 0 28 0;
|
|
r@244
|
938 #X connect 80 0 81 0;
|
|
r@244
|
939 #X connect 81 0 82 0;
|
|
r@244
|
940 #X connect 83 0 84 0;
|
|
r@244
|
941 #X connect 86 0 29 0;
|
|
r@244
|
942 #X connect 86 0 4 0;
|
|
r@244
|
943 #X connect 87 0 78 2;
|
|
r@243
|
944 #X connect 89 0 90 0;
|
|
r@244
|
945 #X connect 91 0 92 1;
|
|
r@249
|
946 #X connect 92 0 96 0;
|
|
r@244
|
947 #X connect 93 0 78 3;
|
|
r@244
|
948 #X connect 94 0 79 3;
|
|
r@244
|
949 #X connect 95 0 79 4;
|
|
r@249
|
950 #X connect 96 0 9 0;
|
|
r@251
|
951 #X connect 98 0 76 0;
|
|
r@275
|
952 #X connect 99 0 100 0;
|
|
r@275
|
953 #X connect 100 0 101 0;
|
