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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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417 #X text -20627 194 Angle goes with the flow in Goldstein hence 90 -
|
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r@196
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418 theta so that theta is same angle as dipole angles.;
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479 #X restore 108 567 pd GoldnoiseGain;
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480 #X text 99 614 Calculates the gain of the wake;
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487 #X text 234 22 Y = 10^b . X^m;
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488 #X text 235 40 b = 1.536;
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r@196
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490 #X text 80 297 Equation of line derived from Norberg 2001;
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509 #X text 484 537 the object and environment;
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522 #X obj 201 542 r~ \$0-elev;
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523 #N canvas 339 112 976 679 Dipoles 0;
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525 #X obj 91 107 r~ \$0-liftDiGain;
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526 #X obj 353 69 r~ \$0-myFreq;
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527 #X obj 368 135 r~ \$0-liftDiGain;
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|
529 #X obj 621 62 r~ \$0-myFreq;
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530 #X obj 636 125 r~ \$0-liftDiGain;
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531 #X obj 621 86 *~ 5;
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536 #X obj 494 358 r~ \$0-myFreq;
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541 #X obj 210 264 throw~ l;
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542 #X obj 237 241 throw~ r;
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543 #X obj 210 220 fcpan;
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545 #X obj 237 198 r \$0-thisPan;
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547 #X obj 480 192 *~;
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548 #X obj 480 257 throw~ l;
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549 #X obj 507 234 throw~ r;
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550 #X obj 480 213 fcpan;
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555 #X obj 750 248 throw~ l;
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556 #X obj 777 225 throw~ r;
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557 #X obj 750 204 fcpan;
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559 #X obj 777 182 r \$0-thisPan;
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560 #X obj 750 65 r~ \$0-thisNoise;
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562 #X obj 360 478 *~;
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563 #X obj 360 543 throw~ l;
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564 #X obj 387 520 throw~ r;
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r@196
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565 #X obj 360 499 fcpan;
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|
566 #X obj 360 402 vcf~ 3;
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r@196
|
567 #X obj 387 477 r \$0-thisPan;
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|
568 #X obj 360 358 r~ \$0-thisNoise;
|
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|
569 #X obj 634 476 *~;
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570 #X obj 634 541 throw~ l;
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571 #X obj 661 518 throw~ r;
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572 #X obj 634 497 fcpan;
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574 #X obj 661 475 r \$0-thisPan;
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|
r@196
|
575 #X obj 634 358 r~ \$0-thisNoise;
|
|
r@196
|
576 #X text 273 27 Generates the sound associated with the lift dipole.
|
|
r@196
|
577 ;
|
|
r@196
|
578 #X text 318 326 Generates the sound associated with the drag dipole.
|
|
r@196
|
579 ;
|
|
r@196
|
580 #X obj 243 88 r \$0-Qval;
|
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r@196
|
581 #X obj 513 94 r \$0-Qval;
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582 #X obj 783 86 r \$0-Qval;
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593 #X obj 750 131 vcf~ 3;
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612 #X connect 12 0 14 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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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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695 #X obj 219 208 * 4.624e-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@196
|
704 #X text -84 298 First section of the Reynolds number - DeltaF/F relationship
|
|
r@196
|
705 is linear and did not appear to be reliant on current TU values;
|
|
r@196
|
706 #X text 565 329 Third section of the Reynolds number - DeltaF/F relationship
|
|
r@196
|
707 is linear and did not appear to be reliant on current TU values;
|
|
r@196
|
708 #X text 114 -16 Middle section of Reynolds number - DeltaF/F relationship
|
|
r@196
|
709 is also linear but depends on TU Value;
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