brett s
23rd Sep 2008, 12:27
Working on a Bell 206B model for a flight sim (X-Plane), the following info would be very helpful:
Approximate total weight of a main rotor blade, plus amount & location of any tip weight - or even better, the polar moment of inertia for the main rotor.
Approximate main rotor collective pitch range
Tail rotor pitch limitsThanks in advance!
Approximate total weight of a main rotor blade, plus amount & location of any tip weight - or even better, the polar moment of inertia for the main rotor.
Approximate main rotor collective pitch range
Tail rotor pitch limitsThanks in advance!