Analytical Model of Elastomeric Lag Damper Kinematic Coupling and Its Effect on Helicopter Air Resonance in Hover-Reference-Cited by-同舟云学术

Analytical Model of Elastomeric Lag Damper Kinematic Coupling and Its Effect on Helicopter Air Resonance in Hover

Published:2002-02 Issue:1 Volume:15 Page:27-32
ISSN:1000-9361
Container-title:Chinese Journal of Aeronautics
language:en
Short-container-title:Chinese Journal of Aeronautics

Author:

HU Guo-cai,XIANG Jin-wu,ZHANG Xiao-gu

Publisher

Elsevier BV

Subject

Mechanical Engineering,Aerospace Engineering

Reference10 articles.

1. Wang J M. A successful comprehensive rotor dynamics correlation for a Sikorsky fullscale bearingless main rotor [A]. In: The American Helicopter Society 53rd Annual Forum [C]. Virginia Beach, VA, 1997. 1336–1349.

2. Krysinski T, Ferullo D. Overview of the EC155 dynamics validation program from design stage up to certification[A]. In: The American Helicopter Society 55th Annual Forum [C]. Montreal Canada, 1999.

3. Nonlinear behavior of an elastomeric lag damper undergoing dual-frequency motion and its effect on rotor dynamics[J];Felker;Journal of the American Helicopter Society,1987

4. An analytical model for a nonlinear elastomeric lag damper and its effect on aeromechanical stability in hover [J];Gandhi;Journal of the American Helicopter Society,1994

5. Analysis of bearingless main rotor dynamics with the inclusion of an improved time domain nonlinear elastomeric damper model[J];Gandhi;Journal of the American Helicopter Society,1996

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