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309 #X text -21029 218 Mass Density of Air \, squared;
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r@195
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310 #X text -20831 411 Distance;
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r@195
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342 #X text -20915 17 Gain proportional to windspeed to power 8 for spectrum
|
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|
343 ;
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|
344 #X text -20765 146 Diameter;
|
|
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|
345 #X text -20798 63 Wind speed;
|
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|
346 #X text -21027 546 Calculates wake gain;
|
|
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r@195
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385 1;
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412 #X obj -20775 387 *~;
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r@195
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413 #X obj -20775 460 *~;
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414 #X obj -20831 486 *~;
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r@195
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415 #X obj -20846 514 /~;
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r@195
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416 #X obj -20679 187 -~;
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r@195
|
417 #X text -20627 194 Angle goes with the flow in Goldstein hence 90 -
|
|
r@195
|
418 theta so that theta is same angle as dipole angles.;
|
|
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|
419 #X obj -20679 142 sig~ 180;
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420 #X obj -20616 146 r~ \$0-this_elev;
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428 #X obj -20846 294 *~ 2.50663;
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429 #X text -20776 124 Corrolation Length;
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430 #X text -20753 232 Length;
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478 #X connect 51 0 41 1;
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r@195
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479 #X restore 108 567 pd GoldnoiseGain;
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r@195
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480 #X text 99 614 Calculates the gain of the wake;
|
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r@195
|
481 #N canvas 1021 287 444 428 corrLen 0;
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482 #X obj 103 71 inlet~;
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484 #X obj 88 143 *~;
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485 #X obj 124 93 sig~ -0.245;
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r@195
|
486 #X obj 103 119 pow~;
|
|
r@195
|
487 #X text 234 22 Y = 10^b . X^m;
|
|
r@195
|
488 #X text 235 40 b = 1.536;
|
|
r@195
|
489 #X text 235 56 m = -0.245;
|
|
r@195
|
490 #X text 80 297 Equation of line derived from Norberg 2001;
|
|
r@195
|
491 #X obj 88 169 max~ 1;
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497 #X connect 9 0 1 0;
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498 #X connect 10 0 2 0;
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r@195
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499 #X restore 966 94 pd corrLen Calc;
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r@195
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500 #X obj 966 118 s~ \$0-myCor;
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r@195
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501 #X obj 156 237 r~ \$0-myCor;
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r@195
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502 #X obj 787 324 hip~;
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r@195
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503 #X obj 154 481 r~ \$0-myCor;
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r@195
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504 #X obj 646 91 max 0.01;
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r@195
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505 #X obj 646 114 min 0.99;
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r@195
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506 #X obj 1076 69 noise~;
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r@195
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507 #X obj 1076 92 s~ \$0-thisNoise;
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r@195
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508 #X obj 787 229 r~ \$0-thisNoise;
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r@195
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509 #X text 484 537 the object and environment;
|
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r@195
|
510 #X obj 130 75 inlet~;
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r@195
|
511 #X obj 398 71 inlet~;
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r@195
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512 #X obj 403 94 s~ \$0-dist;
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r@195
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513 #X obj 165 256 r~ \$0-dist;
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r@195
|
514 #X obj 139 459 r~ \$0-dist;
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r@195
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515 #X obj 470 70 inlet~;
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r@195
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516 #X obj 477 92 s~ \$0-azim;
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r@195
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517 #X obj 185 298 r~ \$0-azim;
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r@195
|
518 #X obj 185 522 r~ \$0-azim;
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r@195
|
519 #X obj 544 69 inlet~;
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r@195
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520 #X obj 552 92 s~ \$0-elev;
|
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r@195
|
521 #X obj 175 277 r~ \$0-elev;
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r@195
|
522 #X obj 201 542 r~ \$0-elev;
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r@195
|
523 #N canvas 339 112 976 679 Dipoles 0;
|
|
r@195
|
524 #X obj 76 62 r~ \$0-myFreq;
|
|
r@195
|
525 #X obj 91 107 r~ \$0-liftDiGain;
|
|
r@195
|
526 #X obj 353 69 r~ \$0-myFreq;
|
|
r@195
|
527 #X obj 368 135 r~ \$0-liftDiGain;
|
|
r@195
|
528 #X obj 368 157 *~ 0.6;
|
|
r@195
|
529 #X obj 621 62 r~ \$0-myFreq;
|
|
r@195
|
530 #X obj 636 125 r~ \$0-liftDiGain;
|
|
r@195
|
531 #X obj 621 86 *~ 5;
|
|
r@195
|
532 #X obj 353 93 *~ 3;
|
|
r@195
|
533 #X obj 215 359 r~ \$0-myFreq;
|
|
r@195
|
534 #X obj 230 432 r~ \$0-dragDiGain;
|
|
r@195
|
535 #X obj 215 387 *~ 2;
|
|
r@195
|
536 #X obj 494 358 r~ \$0-myFreq;
|
|
r@195
|
537 #X obj 528 406 r~ \$0-dragDiGain;
|
|
r@195
|
538 #X obj 494 386 *~ 4;
|
|
r@195
|
539 #X obj 528 429 *~ 0.125;
|
|
r@195
|
540 #X obj 210 199 *~;
|
|
r@195
|
541 #X obj 210 264 throw~ l;
|
|
r@195
|
542 #X obj 237 241 throw~ r;
|
|
r@195
|
543 #X obj 210 220 fcpan;
|
|
r@195
|
544 #X obj 210 108 vcf~ 3;
|
|
r@195
|
545 #X obj 237 198 r \$0-thisPan;
|
|
r@195
|
546 #X obj 210 67 r~ \$0-thisNoise;
|
|
r@195
|
547 #X obj 480 192 *~;
|
|
r@195
|
548 #X obj 480 257 throw~ l;
|
|
r@195
|
549 #X obj 507 234 throw~ r;
|
|
r@195
|
550 #X obj 480 213 fcpan;
|
|
r@195
|
551 #X obj 480 116 vcf~ 3;
|
|
r@195
|
552 #X obj 507 191 r \$0-thisPan;
|
|
r@195
|
553 #X obj 480 68 r~ \$0-thisNoise;
|
|
r@195
|
554 #X obj 750 183 *~;
|
|
r@195
|
555 #X obj 750 248 throw~ l;
|
|
r@195
|
556 #X obj 777 225 throw~ r;
|
|
r@195
|
557 #X obj 750 204 fcpan;
|
|
r@195
|
558 #X obj 750 107 vcf~ 3;
|
|
r@195
|
559 #X obj 777 182 r \$0-thisPan;
|
|
r@195
|
560 #X obj 750 65 r~ \$0-thisNoise;
|
|
r@195
|
561 #X obj 636 147 *~ 0.1;
|
|
r@195
|
562 #X obj 360 478 *~;
|
|
r@195
|
563 #X obj 360 543 throw~ l;
|
|
r@195
|
564 #X obj 387 520 throw~ r;
|
|
r@195
|
565 #X obj 360 499 fcpan;
|
|
r@195
|
566 #X obj 360 402 vcf~ 3;
|
|
r@195
|
567 #X obj 387 477 r \$0-thisPan;
|
|
r@195
|
568 #X obj 360 358 r~ \$0-thisNoise;
|
|
r@195
|
569 #X obj 634 476 *~;
|
|
r@195
|
570 #X obj 634 541 throw~ l;
|
|
r@195
|
571 #X obj 661 518 throw~ r;
|
|
r@195
|
572 #X obj 634 497 fcpan;
|
|
r@195
|
573 #X obj 634 400 vcf~ 3;
|
|
r@195
|
574 #X obj 661 475 r \$0-thisPan;
|
|
r@195
|
575 #X obj 634 358 r~ \$0-thisNoise;
|
|
r@195
|
576 #X text 273 27 Generates the sound associated with the lift dipole.
|
|
r@195
|
577 ;
|
|
r@195
|
578 #X text 318 326 Generates the sound associated with the drag dipole.
|
|
r@195
|
579 ;
|
|
r@195
|
580 #X obj 243 88 r \$0-Qval;
|
|
r@195
|
581 #X obj 513 94 r \$0-Qval;
|
|
r@195
|
582 #X obj 783 86 r \$0-Qval;
|
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r@195
|
583 #X obj 667 378 r \$0-Qval;
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r@195
|
584 #X obj 393 380 r \$0-Qval;
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r@195
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585 #X obj 210 158 *~ 1;
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r@195
|
586 #X obj 480 159 *~ 1;
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r@195
|
587 #X obj 750 154 *~ 1;
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r@195
|
588 #X obj 634 442 *~ 1;
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r@195
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589 #X obj 360 445 *~ 1;
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r@195
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590 #X floatatom 277 122 5 0 0 0 - - -;
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r@195
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591 #X obj 210 134 vcf~ 3;
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r@195
|
592 #X obj 480 138 vcf~ 3;
|
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r@195
|
593 #X obj 750 131 vcf~ 3;
|
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r@195
|
594 #X obj 634 421 vcf~ 3;
|
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r@195
|
595 #X obj 360 423 vcf~ 3;
|
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r@195
|
596 #X connect 0 0 20 1;
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r@195
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597 #X connect 0 0 65 1;
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r@195
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598 #X connect 1 0 16 1;
|
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r@195
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599 #X connect 2 0 8 0;
|
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r@195
|
600 #X connect 3 0 4 0;
|
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r@195
|
601 #X connect 4 0 23 1;
|
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r@195
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602 #X connect 5 0 7 0;
|
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r@195
|
603 #X connect 6 0 37 0;
|
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r@195
|
604 #X connect 7 0 34 1;
|
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r@195
|
605 #X connect 7 0 67 1;
|
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r@195
|
606 #X connect 8 0 27 1;
|
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r@195
|
607 #X connect 8 0 66 1;
|
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r@195
|
608 #X connect 9 0 11 0;
|
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r@195
|
609 #X connect 10 0 38 1;
|
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r@195
|
610 #X connect 11 0 42 1;
|
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r@195
|
611 #X connect 11 0 69 1;
|
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r@195
|
612 #X connect 12 0 14 0;
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613 #X connect 13 0 15 0;
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668 #X connect 69 0 63 0;
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669 #X restore 774 538 pd Dipoles;
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670 #X obj 32 72 inlet~;
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671 #X obj 32 92 s~ \$0-sourceRe;
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677 -1;
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680 -1 -1;
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685 #X obj 460 391 /;
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686 #X obj 460 342 / 100;
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687 #X obj 461 434 outlet;
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688 #X text 437 453 Q value;
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690 #X obj 477 -14 snapshot~;
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691 #X obj 203 164 spigot;
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692 #X obj 219 187 spigot;
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693 #X obj 236 140 > 0;
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694 #X obj 219 233 + 0.9797;
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695 #X obj 219 208 * 4.624e-05;
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696 #X obj 602 150 spigot;
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697 #X obj 618 173 spigot;
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698 #X obj 651 149 < 1e+06;
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699 #X obj 618 216 * 1.227e-10;
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700 #X obj 618 196 *;
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701 #X obj 690 215 * -8.553e-05;
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702 #X obj 618 261 + 16.5;
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703 #X obj 618 238 +;
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r@195
|
704 #X text -84 298 First section of the Reynolds number - DeltaF/F relationship
|
|
r@195
|
705 is linear and did not appear to be reliant on current TU values;
|
|
r@195
|
706 #X text 565 329 Third section of the Reynolds number - DeltaF/F relationship
|
|
r@195
|
707 is linear and did not appear to be reliant on current TU values;
|
|
r@195
|
708 #X text 114 -16 Middle section of Reynolds number - DeltaF/F relationship
|
|
r@195
|
709 is also linear but depends on TU Value;
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710 #X obj 461 412 max 0.005;
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744 #X restore 1189 82 pd StBandwidth;
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745 #X obj 1189 105 s \$0-Qval;
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746 #X obj 966 71 r~ \$0-sourceRe;
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808 #X connect 93 0 92 0;
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