DocumentCode :
489242
Title :
Damping in Coupled Bending and Torsion - An Experiment
Author :
Umland, Jeffrey W. ; Inman, Daniel J. ; Banks, H.T.
Author_Institution :
Jet Propulsion Laboratory; Mechanical Systems Laboratory, Dept. of Mechanical and Aerospace Eng., University at Buffalo, Buffalo, NY 14260
fYear :
1991
fDate :
26-28 June 1991
Firstpage :
2994
Lastpage :
2999
Abstract :
Traditional experimental modal testing methods are used to determine the damping properties of an Euler-Bernoulli beam with offset inertial tip mass. Both viscous and strain rate damping models are considered in bending and in torsion. A partial differential equation model of the coupled system is used. Eigenfunctions are derived for the coupled system by using a Green´s function approach to derive the approximate uncoupled eigenfunctions. These eigenfunctions are used in a decoupled fashion with experimental modal data to estimate the damping parameters of the coupled system. The experimental modal data was obtained from both free and impulse responses using a combined translational and rotational accelerometer.
Keywords :
Aerodynamics; Aerospace testing; Aluminum; Damping; Eigenvalues and eigenfunctions; Material properties; Parameter estimation; Partial differential equations; System testing; Vibration measurement;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
American Control Conference, 1991
Conference_Location :
Boston, MA, USA
Print_ISBN :
0-87942-565-2
Type :
conf
Filename :
4791952
Link To Document :
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