PPRuNe Forums - View Single Post - VNE of light helicopter, altitude reduction ?
Old 2nd March 2012 | 12:14
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heole
 
Joined: Aug 2004
Posts: 8
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From: Quebec Canada
Hi Sawn.

Indeed!, You a right!

I have seen various other factors for VNE limits, such as critical loads caused by blade stall, Mach tuck, , Tail rotor flapping, dynamic instability, Compressibility, Airframe vibrations or critical loads on stabilisers, excessive feed back, Control margins and sometime regulations.
Leo
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