TheBeardedFatGuy
Birdie Member
I've been trying to understand what the optimal pitch angle for distance should be, and I'd appreciate the input of anyone who can add insight.
It's pretty well accepted that the optimal angle of disc orientation to the plane of flight is -4 degrees - the 'nose down' angle that minimizes drag from lift, but what is the optimal launch angle that establishes that plane of flight and will give maximum distance? If we were dealing more with pure ballistics, as when launching a baseball or cannonball, instead of a spinning disc with very different flight characteristics, the established optimal angle would be 45 degrees. This is the angle that will produce the greatest possible distance. With a disc, however, 45 degrees is a very steep angle, unheard of except when throwing an extreme hyzer/anhyzer bomb or tomahawk. As the red disc in figure D shows, gyroscopic stability tends to keep the disc oriented at the same angle through the arc of it's flight, which presents more of the disc's bottom to the direction of flight, causing it to stall out and die a quick death. If the nose were constantly adjusted to keep the -4 degree orientation to the plane of flight (green disc in figure D), we might be on to something. But, again, that behavior is contrary to gyroscopic stability. I suppose it could still happen if the stability from spin was reduced steadily at just the right rate to allow the disc's airfoil characteristics to win out over gyroscopic stability. In that case, the disc would stay oriented more or less correctly, more lie a thrown paper airplane than a disc, but if you can do that you should be burned at the stake for practicing witchcraft.
(OP continues in next reply...)
It's pretty well accepted that the optimal angle of disc orientation to the plane of flight is -4 degrees - the 'nose down' angle that minimizes drag from lift, but what is the optimal launch angle that establishes that plane of flight and will give maximum distance? If we were dealing more with pure ballistics, as when launching a baseball or cannonball, instead of a spinning disc with very different flight characteristics, the established optimal angle would be 45 degrees. This is the angle that will produce the greatest possible distance. With a disc, however, 45 degrees is a very steep angle, unheard of except when throwing an extreme hyzer/anhyzer bomb or tomahawk. As the red disc in figure D shows, gyroscopic stability tends to keep the disc oriented at the same angle through the arc of it's flight, which presents more of the disc's bottom to the direction of flight, causing it to stall out and die a quick death. If the nose were constantly adjusted to keep the -4 degree orientation to the plane of flight (green disc in figure D), we might be on to something. But, again, that behavior is contrary to gyroscopic stability. I suppose it could still happen if the stability from spin was reduced steadily at just the right rate to allow the disc's airfoil characteristics to win out over gyroscopic stability. In that case, the disc would stay oriented more or less correctly, more lie a thrown paper airplane than a disc, but if you can do that you should be burned at the stake for practicing witchcraft.
(OP continues in next reply...)