Forced Response Analysis of Aerodynamically Asymmetric Cascades
Author:
Publisher
American Institute of Aeronautics and Astronautics
Reference24 articles.
1. The effects of detuning upon the forced vibrations of bladed disks
2. Flutter and Response of a Mistuned Cascade in Incompressible Flow
3. Flutter of Mistuned Turbomachinery Rotors
4. Model Development and Statistical Investigation of Turbine Blade Mistuning
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1. Effect of System Mode and Structural Damping Perturbation on the Mistuned Forced Response and Aerodynamic Damping of Embedded Compressor Rotors;Journal of Engineering for Gas Turbines and Power;2022-12-20
2. Blended Fan Blade Effects on Unsteady Aerodynamics;AIAA Scitech 2020 Forum;2020-01-05
3. Mapped Chebyshev Pseudo-Spectral Method for Dynamic Aero-Elastic Problem of Limit Cycle Oscillation;International Journal of Aeronautical and Space Sciences;2018-05-07
4. The Impact of Blade Loading and Unsteady Pressure Bifurcations on Low-Pressure Turbine Flutter Boundaries;Journal of Turbomachinery;2015-12-29
5. Forced Response Sensitivity of a Mistuned Rotor From an Embedded Compressor Stage;Journal of Turbomachinery;2015-11-17
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