Sorry Gaseous,
I have never heard of of that term "pilot induced LTE". I understand the aerodynamics of LTE or loss of tail rotor effectiveness and all other factors surrounding it.
I agree the tail rotor is less effective due to low Main Rotor Rpm, but surely this is not the same as LTE?
Would you be so kind as to explain your terminology?
Keen to learn something new, so fire away! (and sorry for hijacking the thread)
