David
Joined: 27 Jan 2006 Posts: 3 Location: Bremerton, WA
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| Posted: Fri Feb 03, 2006 11:20 pm Post subject: Blade flapping |
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I have a question regarding blade flapping, the definition of it is as follows:
Blade Flapping is the up and down movement of a rotor blade, which, in conjunction with cyclic feathering, causes Dissymmetry of Lift to be eliminated.
The advancing blade, upon meeting the progressively higher airspeeds brought about by the addition of forward flight velocity to the rotational airspeed (of the rotor), responds to the increase of speed by producing more lift.
The blade flaps (or climbs) upward, and the change in relative wind and angle of attack reduces the amount that would have been generated.
This definition was obtained from the following web address:
http://www.dynamicflight.com/aerodynamics/flapping/
My question is: is blade flapping a common problem encountered or is it something that you just have to be consciensously aware of as forward velocity increases? Also I am not very sure what the current Army rotor blades are made out of, but would it help at all to place lead weights at the tips like they do on the carter copters? I'm just curious, because they have been having good results with this. Thank you for your help.
V/r
David |
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