Flutter Computation of Turbomachinery Cascades Using a Parallel Unsteady Navier-Stokes Code
Author:
Affiliation:
1. University of California, Irvine, Irvine, California 92697-3975
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.733
Reference28 articles.
1. Coupled Blade-Disk-Shroud Flutter Instabilities in Turbojet Engine Rotors
2. Smith, S. N. “Discrete Frequency Sound Generation in Axial Flow Turbomachines,” Ph.D. Dissertation, Engineering Dept.Cambridge Univ., Cambridge, England, UK,1971.
3. A linearized unsteady aerodynamic analysis for transonic cascades
4. Numerical Analysis of Fully Three-Dimensional Periodic Flows Through a Turbine Stage
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