PPRuNe Forums - View Single Post - Turbulators on Helicopter Blades ?

25th Jan 2005, 14:01

#11 (permalink)

Thomas coupling

Join Date: Aug 2000

Location: UK

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Zeeoo: you could consider postulating the disturbed flow under the nacelles and wingform.
This gives optimised non laminer flow without degradation of theta2.
try a reynolds number equivalent to the latest NACA series amendment?

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