Integrally Bladed Rotor Mistuning Identification and Model Updating Using Geometric Mistuning Models
Author:
Affiliation:
1. Perceptive Engineering Analytics, Minneapolis, MN 55418
2. AFRL Turbine Engine Division, Wright-Patterson AFB, OH 45433
3. Advanced Engineering Solutions, Lafayette, CO 80026
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/143/12/121012/6770417/gtp_143_12_121012.pdf
Reference25 articles.
1. Testing and Calibration Procedures for Mistuning Identification and Traveling Wave Excitation of Blisks;ASME J. Eng. Gas Turbines Power,2010
2. Next Generation Traveling-Wave Excitation System for Integrally Bladed Rotors;J. Aerosp. Eng.,2015
3. Identification of Mistuning Characteristics of Bladed Disks From Free Response Data—Part I;ASME J. Eng. Gas Turbines Power,2001
4. Mistuning Identification of Bladed Disks Using a Fundamental Mistuning Model—Part I: Theory;ASME J. Turbomach.,2004
5. Reduced-Order Model Construction Procedure for Robust Mistuning Identification of Blisks;AIAA J.,2008
Cited by 1 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献
1. Modal Identification for Integrally Bladed Rotors Under Traveling Wave Excitation;Journal of Engineering for Gas Turbines and Power;2023-01-13
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