Nemesis_Vibration

Working Papers:

DESIGN:

A112

MAKE:

BUY:

Secondary Grouping:

	Rotor Induced - Analysis:
	Rotor Induced - Control:
	Engine Induced	See: OTHER: Mechanics - Vibration - Engine Induced

Notes (to be eventually moved to sub pages):

During hover the retreating tip at 270º azimuth will be over the other rotor's spar. This may result in a lateral vibration from the downwash on the spar followed by an opposite motion due to the reaction on the blade???

Same Page ~ Different Craft: ~ SynchroLite, UniCopter

Last Revised: March 21, 2007