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RESEARCH PAPERS: Turbomachinery Vibrations

Coupling Technique of Rotor-Fuselage Dynamic Analysis

[+] Author and Article Information
D. M. Tang, M. Q. Wang

Nanjing Aeronautical Institute, Nanjing, China

J. Vib., Acoust., Stress, and Reliab 106(2), 235-238 (Apr 01, 1984) (4 pages) doi:10.1115/1.3269174 History: Received June 10, 1983; Online November 23, 2009

Abstract

In this paper is introduced a method of dynamic analysis of the helicopter rotor coupled with fuselage in the rotating plane. The method has been used to determine the inplane rotor-fuselage dynamic properties of a light helicopter with fiberglass-reinforced plastics rotor blades. This paper makes particular reference to the effect of anisotropic dynamic stiffness of the rotor shaft end of fuselage on the natural dynamic characteristics.

Copyright © 1984 by ASME
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