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TECHNICAL PAPERS

Maximum Bladed Disk Forced Response From Distortion of a Structural Mode

[+] Author and Article Information
J. A. Kenyon

Propulsion Directorate, Air Force Research Laboratory, Wright-Patterson AFB, OH 45433

J. H. Griffin, D. M. Feiner

Department of Mechanical Engineering, Carnegie Mellon University, Pittsburgh, PA 15213e-mail: dfein@andrew.cmu.edu

J. Turbomach 125(2), 352-363 (Apr 23, 2003) (12 pages) doi:10.1115/1.1540118 History: Received January 30, 2002; Online April 23, 2003
Copyright © 2003 by ASME
Topics: Damping , Disks , Blades
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References

Figures

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Mass-spring-damper system
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Localization of mode for maximum response
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Forced response simulation of intentionally mistuned system
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Probability distribution of response for intentionally mistuned system
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Reduction in sensitivity for intentionally mistuned systems with simple damping
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Forced response using Whitehead formulation
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Comparison of mode shapes for maximum response

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