Component-Mode Reduced-Order Models for Geometric Mistuning of Integrally Bladed Rotors
Author:
Affiliation:
1. Aerospace Systems Directorate, U.S. Air Force Research Laboratory, Wright–Patterson Air Force Base, Ohio 45433
2. Department of Mechanical and Materials Engineering, Wright State University, Dayton, Ohio 45435
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J052420
Reference33 articles.
1. Dynamics of rotationally periodic structures
2. Methods that combine finite group theory with component mode synthesis in the analysis of repetitive structures
3. A Reduced Order Modeling Technique for Mistuned Bladed Disks
4. A Reduced-Order Model of Mistuning Using a Subset of Nominal System Modes
5. A Reduced Order Approach for the Vibration of Mistuned Bladed Disk Assemblies
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