I am running analysis in Profili and it's asking me about Reynolds numbers. Can anyone help me figure this out. I keep coming up with 500K as the number but in discussions in this section I keep seeing 1000K as the number. Which one is it?
I used the following calculator:
http://aero.stanford.edu/StdAtm.htmlI used 80ft/sec speed which is equivalent 55mph which is equivalent to 5.2 second laps with 63 ft lines.
I left 1ft for the chord and tried smaller numbers with little change
I used 1000ft MSL as the altitude.
The calculator gave me 496742.40
Am I doing something wrong or is 500K the right number?