to Lu Zuckerman: I followed the link and under Frank Robinsons comments it gave a summation of your position. In it you said that one of your fears was when a pilot encountered a low-g if they pulled aft cyclic they could exacerbate the roll.
ok so my first question is what would be the correct cyclic application? would it be to go slightly aft and slightly left cyctic? another thing that i have wondered is what an increase in the collective would do to reload the rotor? what are the problems that i havent foreseen with increasing the collective to reload the rotor.
ok so that was actually 2 questions but i have one more as well.
Why didnt robinson design the rotor system like the bell 2 blade heads?
all of the posts have been really informative and interesting, I appreciate any answers to my questions. thanks you