Effect of Fuselage Dynamics on Helicopter Ground Resonance: Investigation of the Influence of Dynamic Properties on the Rotor to Fuselage Effective Mass Ratio and its Effect on Stability Boundaries

Author: A.F.R.Ae.S. W.E. Hooper   M.A.   A.M.I.Mech.E.  

Publisher: Emerald Group Publishing Ltd

ISSN: 0002-2667

Source: Aircraft Engineering, Vol.34, Iss.8, 1993-12, pp. : 226-230

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Abstract