Testing and Calibration Procedures for Mistuning Identification and Traveling Wave Excitation of Blisks
Author:
Affiliation:
1. Department of Mechanical Engineering, University of Michigan, Ann Arbor, MI 48109
2. Aeromechanics Technology, GE Advanced Mechanical Design, Cincinnati, OH 45245
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/132/4/042502/6739761/042502_1.pdf
Reference27 articles.
1. Flutter and Resonant Vibration Characteristics of Engine Blades;Srinivasan;ASME J. Eng. Gas Turbines Power
2. Forced Response of Bladed Disk Assemblies—A Survey;Slater;Shock Vib. Dig.
3. Modeling and Analysis of Mistuned Bladed Disk Vibration: Status and Emerging Directions;Castanier;J. Propul. Power
4. The National Turbine Engine High Cycle Fatigue Program;Thomson;The Global Gas Turbine Newsletter (GGTN)
5. Experimental Identification of Mistuning in Blisks;Judge
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