• 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