diff scene demo/freqCalcCyl4No_D4Mach.pd @ 214:18d9eb604d30

Propellor model: Added second blad, angle calcs and doppler effect

Scene: Back up running, WIRES ONLY

--- /dev/null	Thu Jan 01 00:00:00 1970 +0000
+++ b/scene demo/freqCalcCyl4No_D4Mach.pd	Thu Apr 07 12:59:11 2016 +0100
@@ -0,0 +1,1195 @@
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+#X text 285 599 Calculates the gain of the wake;
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+#X text 234 22 Y = 10^b . X^m;
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+#X text 235 56 m = -0.245;
+#X text 80 297 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 175 312 Generates the sound associated with the drag dipole.
+;
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+#X text 674 440 the object and environment;
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+#X text 223 3 Peak dependant on TU value;
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+#X text 548 50 Calculates the peak value of DeltaF / F depending on
+the TU values. The higher the TU the higher the DeltaF/F value. A limit
+of 200 has been made as the value is a % and bandwidth greater than
+200% would invlove -ve frequencies;
+#X text -9 102 Linear up slope of the second section;
+#X text 478 174 Linear down slope of the second section;
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+#X text -84 298 First section of the Reynolds number - DeltaF/F relationship
+is linear and did not appear to be reliant on current TU values;
+#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
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