Application of Symmetry Property for Transient Response Analysis of Mistuned Bladed Disks
Author:
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2016-4957
Reference20 articles.
1. Modeling and Analysis of Mistuned Bladed Disk Vibration: Current Status and Emerging Directions
2. A Statistical Characterization of the Effects of Mistuning in Multistage Bladed Disks
3. Two efficient staggered algorithms for the serial and parallel solution of three-dimensional nonlinear transient aeroelastic problems
4. Provably second-order time-accurate loosely-coupled solution algorithms for transient nonlinear computational aeroelasticity
5. A Fundamental Model of Mistuning for a Single Family of Modes
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