0
TECHNICAL PAPERS: Gas Turbines: Structures and Dynamics

Forced Response of Turbine Engine Bladed Disks and Sensitivity to Harmonic Mistuning

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

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

J. H. Griffin

Department of Mechanical Engineering, Carnegie Mellon University, 5000 Forbes Avenue, Pittsburgh, PA 15213

J. Eng. Gas Turbines Power 125(1), 113-120 (Dec 27, 2002) (8 pages) doi:10.1115/1.1498269 History: Received December 01, 2000; Revised March 01, 2001; Online December 27, 2002
Copyright © 2003 by ASME
Your Session has timed out. Please sign back in to continue.

References

Figures

Grahic Jump Location
Maximum amplitude magnification as a function of number of harmonics
Grahic Jump Location
Reduction in sensitivity near worst-case mistuning
Grahic Jump Location
Circular ring with a continuous ring-to-ground shear spring
Grahic Jump Location
Discrete mass-spring model of bladed disks
Grahic Jump Location
Mistuned response sensitivity curves
Grahic Jump Location
The effects of various terms on the solution for splitting modes
Grahic Jump Location
Forced response approximation for nonsplitting modes

Tables

Errata

Discussions

Some tools below are only available to our subscribers or users with an online account.

Related Content

Customize your page view by dragging and repositioning the boxes below.

Related Journal Articles
Related eBook Content
Topic Collections

Sorry! You do not have access to this content. For assistance or to subscribe, please contact us:

  • TELEPHONE: 1-800-843-2763 (Toll-free in the USA)
  • EMAIL: asmedigitalcollection@asme.org
Sign In