Geometric Mistuning Identification of Integrally Bladed Rotors Using Modified Modal Domain Analysis
Author:
Affiliation:
1. ANSYS, Inc., Canonsburg, PA 15317 e-mail:
2. Department of Mechanical and Nuclear Engineering, The Pennsylvania State University, University Park, PA 16802 e-mail:
Abstract
Publisher
ASME International
Subject
Mechanical Engineering,Energy Engineering and Power Technology,Aerospace Engineering,Fuel Technology,Nuclear Energy and Engineering
Link
http://asmedigitalcollection.asme.org/gasturbinespower/article-pdf/doi/10.1115/1.4027762/6164007/gtp_136_12_122504.pdf
Reference12 articles.
1. Effect of Mistuning on the Vibration of Turbomachinery Blades Induced by Wakes;J. Mech. Eng. Sci.,1966
2. Identification of Mistuning Characteristics of Bladed Disks From Free Response Data—Part I;ASME J Gas Turbines Power,2001
3. Identification of Mistuning Characteristics of Bladed Disks From Free Response Data—Part II;ASME J Gas Turbines Power,2001
4. Lim, S. H., Pierre, C., and Castanier, M. P., 2004, “Mistuning Identification and Reduced-Order Model Updating for Bladed Disks on a Component Mode Mistuning Technique,” 9th National Turbine Engine High Cycle Fatigue Conference, Pinehurst, NC, March 16–19.
5. Mistuning Identification of Bladed Disks Using a Fundamental Mistuning Model—Part 1: Theory;ASME J. Turbomach.,2004
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