Forced Response Analysis of a Mistuned Blisk Using Noncyclic Reduced-Order Models
Author:
Affiliation:
1. Royal Institute of Technology, 100 44 Stockholm, Sweden
2. GKN Aerospace Sweden AB, 461 81 Trollhättan, Sweden
3. Siemens Energy Inc., Orlando, Florida 32817
4. University of Stuttgart, 70569 Stuttgart, Germany
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.B36584
Reference17 articles.
1. Stability Increase of Aerodynamically Unstable Rotors Using Intentional Mistuning
2. MayorcaM. A. “Numerical Methods for Turbomachinery Aeromechanical Predictions,” Ph.D. Thesis, Royal Inst. of Technology, Stockholm, 2011.
3. Compact, Generalized Component Mode Mistuning Representation for Modeling Bladed Disk Vibration
4. Component-Mode-Based Reduced Order Modeling Techniques for Mistuned Bladed Disks—Part I: Theoretical Models
5. Component-Mode-Based Reduced Order Modeling Techniques for Mistuned Bladed Disks—Part II: Application
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3. Nonlinear and dual-parameter chaotic vibrations of lumped parameter model in blisk under combined aerodynamic force and varying rotating speed;Nonlinear Dynamics;2022-02-21
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