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1 #N canvas 356 61 1370 784 10;
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2 #X text 587 178 Mass Density of Air;
|
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3 #X obj 709 179 *~ 1.225;
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4 #X obj 709 254 /~ 1.81e-05;
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5 #X obj 709 209 *~ 1;
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|
6 #X obj 709 372 /~ 1;
|
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7 #X obj 709 348 *~;
|
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8 #X obj 223 63 inlet;
|
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|
9 #X text 742 298 Reynolds Number;
|
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|
10 #X text 589 365 Strouhal Number;
|
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|
11 #X text 739 234 Viscosity;
|
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|
12 #X obj 230 86 s \$0-diameter;
|
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|
13 #X obj 770 178 r \$0-diameter;
|
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14 #X obj 777 353 r \$0-diameter;
|
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15 #X obj 709 441 s~ \$0-myFreq;
|
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16 #X obj 1052 334 *~;
|
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17 #X obj 722 278 s~ \$0-myRey;
|
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18 #X obj 636 57 inlet;
|
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19 #X floatatom 581 126 8 0 0 0 - - -;
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20 #X text 673 460 Calculates the frequency;
|
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|
21 #X text 674 472 based on the physics of;
|
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|
22 #X obj 365 519 r \$0-diameter;
|
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|
23 #X text 297 391 Calculates the gain of the dipole source;
|
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|
24 #X text 490 30 Azimuth;
|
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|
25 #X text 641 39 Pan;
|
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26 #X text 413 29 Elevation;
|
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|
27 #X text 344 32 Distance;
|
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|
28 #X text 218 42 Diameter;
|
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|
29 #X obj 709 319 newStrou;
|
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30 #X floatatom 223 107 0 0 0 0 - - -;
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31 #X obj 1052 403 throw~ l;
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32 #X obj 1079 381 throw~ r;
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33 #X obj 1052 359 fcpan;
|
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|
34 #X obj 431 345 s~ \$0-dragDiGain;
|
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35 #X obj 344 365 s~ \$0-liftDiGain;
|
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36 #X obj 326 454 r~ \$0-str;
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37 #X obj 326 651 s~ \$0-liftNoiseGain;
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38 #X obj 609 350 s~ \$0-str;
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39 #X obj 636 126 s \$0-thisPan;
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40 #X obj 1052 190 r~ \$0-liftNoiseGain;
|
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41 #X obj 1079 334 r \$0-thisPan;
|
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|
42 #X text 1033 164 Noise spectrum calculation;
|
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|
43 #X obj 1067 282 hip~;
|
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44 #X obj 1067 237 rpole~ 0.99;
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45 #X obj 368 194 r \$0-diameter;
|
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46 #X obj 344 147 r~ \$0-str;
|
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47 #X text 317 670 Calculates the gain of the wake;
|
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|
48 #N canvas 1021 287 444 428 corrLen 0;
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49 #X obj 103 71 inlet~;
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50 #X obj 88 200 outlet~;
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51 #X obj 88 143 *~;
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52 #X obj 124 93 sig~ -0.245;
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53 #X obj 103 119 pow~;
|
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|
54 #X text 234 22 Y = 10^b . X^m;
|
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|
55 #X text 235 40 b = 1.536;
|
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|
56 #X text 235 56 m = -0.245;
|
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|
57 #X text 80 297 Equation of line derived from Norberg 2001;
|
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|
58 #X obj 88 169 max~ 1;
|
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59 #X obj 88 46 sig~ 44.67;
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60 #X connect 0 0 4 0;
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61 #X connect 2 0 9 0;
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63 #X connect 4 0 2 1;
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64 #X connect 9 0 1 0;
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65 #X connect 10 0 2 0;
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66 #X restore 708 61 pd corrLen Calc;
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67 #X obj 708 38 r~ \$0-myRey;
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68 #X obj 708 85 s~ \$0-myCor;
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69 #X obj 393 237 r~ \$0-myCor;
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70 #X obj 1067 309 hip~;
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71 #X obj 352 498 r~ \$0-myCor;
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72 #X obj 636 81 max 0.01;
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73 #X obj 636 104 min 0.99;
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74 #N canvas 93 119 976 679 Dipoles 0;
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75 #X obj 131 67 r~ \$0-myFreq;
|
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76 #X obj 225 178 r~ \$0-liftDiGain;
|
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|
77 #X obj 389 58 r~ \$0-myFreq;
|
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|
78 #X obj 528 138 r~ \$0-liftDiGain;
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|
79 #X obj 528 159 *~ 0.6;
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80 #X obj 657 57 r~ \$0-myFreq;
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81 #X obj 798 130 r~ \$0-liftDiGain;
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82 #X obj 657 81 *~ 5;
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83 #X obj 389 82 *~ 3;
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84 #X obj 258 385 r~ \$0-myFreq;
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85 #X obj 371 472 r~ \$0-dragDiGain;
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86 #X obj 258 407 *~ 2;
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87 #X obj 528 385 r~ \$0-myFreq;
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88 #X obj 658 447 r~ \$0-dragDiGain;
|
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89 #X obj 528 413 *~ 4;
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90 #X obj 658 470 *~ 0.125;
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91 #X obj 210 199 *~;
|
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92 #X obj 210 264 throw~ l;
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93 #X obj 237 241 throw~ r;
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94 #X obj 210 220 fcpan;
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95 #X obj 210 108 vcf~ 3;
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96 #X obj 237 198 r \$0-thisPan;
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97 #X obj 210 67 r~ \$0-thisNoise;
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|
98 #X obj 480 192 *~;
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99 #X obj 480 257 throw~ l;
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100 #X obj 507 234 throw~ r;
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101 #X obj 480 213 fcpan;
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102 #X obj 480 116 vcf~ 3;
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103 #X obj 507 191 r \$0-thisPan;
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104 #X obj 480 68 r~ \$0-thisNoise;
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105 #X obj 750 183 *~;
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106 #X obj 750 248 throw~ l;
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107 #X obj 777 225 throw~ r;
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108 #X obj 750 204 fcpan;
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109 #X obj 750 107 vcf~ 3;
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110 #X obj 777 182 r \$0-thisPan;
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111 #X obj 750 65 r~ \$0-thisNoise;
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112 #X obj 798 152 *~ 0.1;
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113 #X obj 338 505 *~;
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114 #X obj 338 570 throw~ l;
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115 #X obj 365 547 throw~ r;
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116 #X obj 338 526 fcpan;
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117 #X obj 338 429 vcf~ 3;
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118 #X obj 365 504 r \$0-thisPan;
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119 #X obj 338 385 r~ \$0-thisNoise;
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120 #X obj 612 503 *~;
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121 #X obj 612 568 throw~ l;
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122 #X obj 639 545 throw~ r;
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123 #X obj 612 524 fcpan;
|
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124 #X obj 612 427 vcf~ 3;
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125 #X obj 639 502 r \$0-thisPan;
|
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|
126 #X obj 612 385 r~ \$0-thisNoise;
|
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|
127 #X text 273 27 Generates the sound associated with the lift dipole.
|
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|
128 ;
|
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|
129 #X text 296 353 Generates the sound associated with the drag dipole.
|
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|
130 ;
|
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|
131 #X obj 270 87 r \$0-Qval;
|
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|
132 #X obj 530 92 r \$0-Qval;
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133 #X obj 800 87 r \$0-Qval;
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134 #X obj 658 406 r \$0-Qval;
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135 #X obj 383 407 r \$0-Qval;
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137 #X obj 480 159 *~ 1;
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138 #X obj 750 154 *~ 1;
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139 #X obj 612 469 *~ 1;
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140 #X obj 338 472 *~ 1;
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141 #X floatatom 277 122 5 0 0 0 - - -;
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142 #X obj 210 131 vcf~ 3;
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144 #X obj 750 130 vcf~ 3;
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145 #X obj 612 449 vcf~ 3;
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215 #X connect 66 0 60 0;
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216 #X connect 67 0 61 0;
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217 #X connect 68 0 62 0;
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218 #X connect 69 0 63 0;
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219 #X restore 649 549 pd Dipoles;
|
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220 #X obj 813 37 noise~;
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221 #X obj 813 60 s~ \$0-thisNoise;
|
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222 #X obj 1067 214 r~ \$0-thisNoise;
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223 #X text 674 485 the object and environment;
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224 #N canvas 308 58 1027 635 StBandwidth 0;
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225 #X obj 460 365 swap 1;
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226 #X obj 460 391 /;
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227 #X obj 460 342 / 100;
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228 #X obj 461 434 outlet;
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229 #X text 437 453 Q value;
|
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231 #X obj 477 -36 r myMet;
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232 #X obj 477 -14 snapshot~;
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233 #X obj 203 164 spigot;
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234 #X obj 219 187 spigot;
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235 #X obj 236 140 > 0;
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236 #X obj 219 233 + 0.9797;
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237 #X obj 219 208 * 4.624e-05;
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238 #X obj 602 150 spigot;
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239 #X obj 618 173 spigot;
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240 #X obj 651 149 < 1e+06;
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241 #X obj 618 216 * 1.227e-10;
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242 #X obj 618 196 *;
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243 #X obj 690 215 * -8.553e-05;
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244 #X obj 618 261 + 16.5;
|
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245 #X obj 618 238 +;
|
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|
246 #X text -84 298 First section of the Reynolds number - DeltaF/F relationship
|
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|
247 is linear and did not appear to be reliant on current TU values;
|
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|
248 #X text 565 329 Third section of the Reynolds number - DeltaF/F relationship
|
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|
249 is linear and did not appear to be reliant on current TU values;
|
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|
250 #X text 114 -16 Middle section of Reynolds number - DeltaF/F relationship
|
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|
251 is also linear but depends on TU Value;
|
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|
252 #X obj 461 412 max 0.005;
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253 #X obj 635 126 > 193260;
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254 #X obj 252 163 < 193260;
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290 #X connect 29 0 2 0;
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291 #X restore 914 59 pd StBandwidth;
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293 #X obj 1153 257 r myMet;
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294 #X obj 1143 278 snapshot~;
|
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295 #X obj 1143 237 r~ \$0-myFreq;
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296 #X text 130 41 Source Speed;
|
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|
297 #X obj 348 51 inlet~;
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298 #X obj 420 50 inlet~;
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299 #X obj 494 49 inlet~;
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300 #X obj 348 72 s~ \$0-dist;
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301 #X obj 117 65 inlet~;
|
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302 #X obj 49 88 /~ 343.56;
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303 #X obj 49 111 s~ \$0-MY_MACH;
|
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|
304 #X obj 406 258 r~ \$0-dist;
|
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|
305 #X obj 418 279 r~ \$0-elev;
|
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|
306 #X obj 431 300 r~ \$0-azim;
|
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|
307 #X obj 419 602 r~ \$0-elev;
|
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|
308 #X obj 405 583 r~ \$0-azim;
|
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|
309 #X obj 392 562 r~ \$0-dist;
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310 #X obj 356 171 r~ \$0-sourceSpeed;
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|
311 #X obj 117 85 s~ \$0-sourceSpeed;
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312 #X obj 709 151 r~ \$0-sourceSpeed;
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313 #X obj 339 476 r~ \$0-sourceSpeed;
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314 #X obj 776 330 r~ \$0-sourceSpeed;
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|
315 #N canvas 51 317 823 563 doppler 0;
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316 #X obj 88 329 inlet~;
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|
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|
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|
318 #X obj 125 141 /~ 360;
|
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|
319 #X obj 110 95 r~ \$0-sourceSpeed;
|
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|
320 #X obj 125 163 cos~;
|
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|
321 #X obj 110 184 *~;
|
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|
322 #X obj 286 114 atan;
|
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|
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327 #X msg 286 161 \$1 15;
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333 #X obj 149 232 *~ -1;
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334 #X obj 110 211 spigot~;
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337 #X obj 141 411 /~;
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r@214
|
338 #X obj 88 435 *~;
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r@214
|
339 #X obj 333 267 r myMet;
|
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|
340 #X text 423 61 Calculate the azimuth angle from the projected position
|
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r@214
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728 theta so that theta is same angle as dipole angles.;
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