MauleSkinner
Well-known member
- Joined
- Sep 4, 2005
- Posts
- 638
So...do you know why a lazy-8 can be flown perfectly with elevator input for only the first 45 degrees of turn for each half of the 8, and no aileron input after about the 95-degree point (just after starting the wings towards level) of each half of the 8.
I'll give you a hint...it involves static stability, dynamic stability, dihedral, pendulum effect, inertia,....
IMO, this is one of the big reasons to have this maneuver in the commercial PTS.
Fly safe!
David
I'll give you a hint...it involves static stability, dynamic stability, dihedral, pendulum effect, inertia,....
IMO, this is one of the big reasons to have this maneuver in the commercial PTS.
Fly safe!
David