Harmonic Balance Analysis of Limit Cycle Oscillations in Turbomachinery
Author:
Affiliation:
1. University of Tennessee, Knoxville, Tennessee 37996-2030
2. Duke University, Durham, North Carolina 27708-0300
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.J050858
Reference19 articles.
1. Fluid/Structure Coupled Aeroelastic Computations for Transonic Flows in Turbomachinery
2. Computation of cascade flutter by uncoupled and coupled methods
3. Efficient Approach for Analysis of Unsteady Viscous Flows in Turbomachines
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