Flutter stability of a rotor blade
Flutter stability of a rotor blade
(OP)
I am interested in the potential risk of flutter in a composite rotorblade that will be very rigid and resistant to in-plane and out-of-plane bending [carbon tow in the spanwise direction], but will be quite flexible in respect to rotation about the pitch axis [fiberglass tow in the chordwise direction].
Any information or comments on this subject will be much appreciated.
Thanks,
Dave Jackson
Any information or comments on this subject will be much appreciated.
Thanks,
Dave Jackson