Forced response of mistuned bladed disks using reduced-order modeling
Author:
Affiliation:
1. Michigan, Univ., Ann Arbor
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1996-1545
Reference9 articles.
1. Localization Phenomena in Mistuned Assemblies with Cyclic Symmetry Part I: Free Vibrations
2. Dynamic response of an industrial turbomachinery rotor
3. A reduced-order modeling technique for mistuned bladed disks
4. Forced Vibrations of a Single Stage Axial Compressor Rotor
5. Model Development and Statistical Investigation of Turbine Blade Mistuning
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1. Robust dynamic analysis of detuned-mistuned rotating bladed disks with geometric nonlinearities;Computational Mechanics;2019-11-12
2. Experimental modal identification of mistuning in an academic two-stage drum;Mechanical Systems and Signal Processing;2017-05
3. Identification of mistuning and model updating of an academic blisk based on geometry and vibration measurements;Mechanical Systems and Signal Processing;2016-02
4. A Reduced-Order Meshless Energy Model for the Vibrations of Mistuned Bladed Disks—Part I: Theoretical Basis;Journal of Turbomachinery;2013-09-13
5. Experimental Mistuning Identification in Bladed Disks Using a Component-Mode-Based Reduced-Order Model;AIAA Journal;2009-05
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