PPRuNe Forums - View Single Post - Bell 206: JetRanger and LongRanger

12th Aug 2004, 09:15

#380 (permalink)

that chinese fella

Join Date: Dec 2003

Location: Australia

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Interesting.......

I had been taught that this limit was due to Main Rotor blade stresses ie. big changes in AofA with resultant big movement of Centre of Pressure and associated loads / stress.

Any thoughts?

TCF

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