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.
Tek-Tips is the largest IT community on the Internet today!
Members share and learn making Tek-Tips Forums the best source of peer-reviewed technical information on the Internet!
-
Congratulations MintJulep on being selected by the Eng-Tips community for having the most helpful posts in the forums last week. Way to Go!
Typical Rotor Blade Behaviour In Flight 1
- Thread starter aerovibe
- Start date
Intermesher
New member
This post certainly does not answer your question, but it is related to the subject mater.
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;
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;
-
1
- #3
- Thread starter
- #4
- Status
Similar threads
- Locked
- Question