A New Experimental Facility for Characterizing Bladed Disk Dynamics at Design Speed
Author:
Affiliation:
1. The Ohio State University, Columbus, Ohio 43210
Funder
Siemens
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference29 articles.
1. Modeling and Analysis of Mistuned Bladed Disk Vibration: Current Status and Emerging Directions
2. A Reduced-Order Model of Mistuning Using a Subset of Nominal System Modes
3. Compact, Generalized Component Mode Mistuning Representation for Modeling Bladed Disk Vibration
4. Reduced-Order Modeling Approach for Blisks with Large Mass, Stiffness, and Geometric Mistuning
5. A Mode-Accelerated XXr (MAX) method for complex structures with large blends
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