Numerical Methods for Calculating Component Modes for Geometric Mistuning Reduced-Order Models
Author:
Affiliation:
1. Perceptive Engineering Analytics, LLC, Minneapolis, MN 55418
2. AFRL/RQTI, 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
https://asmedigitalcollection.asme.org/gasturbinespower/article-pdf/144/3/031006/6807887/gtp_144_03_031006.pdf
Reference38 articles.
1. Component-Mode Reduced-Order Models for Geometric Mistuning of Integrally Bladed Rotors;AIAA J.,2014
2. Geometric Mistuning Reduced-Order Models for Integrally Bladed Rotors With Mistuned Disk-Blade Boundaries;ASME J. Turbomach.,2015
3. Experimental Validation of an Optically Measured Geometric Mistuning Model Using a System ID Approach,2015
4. Modified Modal Domain Analysis of a Bladed Rotor Using Coordinate Measurement Machine Data on Geometric Mistuning;ASME J. Eng. Gas Turbines Power,2015
5. Vibration Modeling of Bladed Disks Subject to Geometric Mistuning and Design Changes,2004
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