Assessment Of The Effectiveness Of A Viscoelastic Damper On The Forced Vibrations Of A Stretched String
Report Number: ML TDR 64-322
Author(s): Jones, D. I. G.
Corporate Author(s): Air Force Materials Lab Wright-Patterson AFB Ohio
Laboratory: AF Materials Laboratory
Date of Publication: 1964-10
Pages: 12
Contract: Laboratory Research - No Contract
DoD Project: 7351 - Metallic Materials
DoD Task: 735106 - Behavior of Metals
Identifier: AD0608383
Abstract:
The behavior of a dynamic damper in a simple structural environment is studied. The structural model used is a stretched string under harmonic loading at the ends. The aim of the analysis is to establish conditions under which maximum damping is obtainable. The unsymmetrical modes are undamped and the analysis is concerned only with the damping of the symmetrical modes.
Provenance: Lockheed Martin Missiles & Fire Control
Author(s): Jones, D. I. G.
Corporate Author(s): Air Force Materials Lab Wright-Patterson AFB Ohio
Laboratory: AF Materials Laboratory
Date of Publication: 1964-10
Pages: 12
Contract: Laboratory Research - No Contract
DoD Project: 7351 - Metallic Materials
DoD Task: 735106 - Behavior of Metals
Identifier: AD0608383
Abstract:
The behavior of a dynamic damper in a simple structural environment is studied. The structural model used is a stretched string under harmonic loading at the ends. The aim of the analysis is to establish conditions under which maximum damping is obtainable. The unsymmetrical modes are undamped and the analysis is concerned only with the damping of the symmetrical modes.
Provenance: Lockheed Martin Missiles & Fire Control