Typical Rotor Blade Behaviour In Flight
Typical Rotor Blade Behaviour In Flight
(OP)
I am writing a report, considering the variations involved in tracking a main rotor blade at the tip, or at the mid section, can anyone point me in the direction of a good diagram displaying how an MRB bends in flight? generic is fine, I realise that numbers of bending modes etc are variable.
RE: Typical Rotor Blade Behaviour In Flight
I am looking into the feasibility of producing and Absolutely Rigid Rotor. The objective is to virtually eliminate flap and lead/lag, leaving only pitch. Theoretically, it should overcome most of the rotors main problems, such as cross-couplings etc. Practicality, may be another story.
If interested, information can be found at; http://www.unicopter.com/0815.html
RE: Typical Rotor Blade Behaviour In Flight
RE: Typical Rotor Blade Behaviour In Flight