Reduced-Order Modeling of Unsteady Viscous Flow in a Compressor Cascade
Author:
Affiliation:
1. 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/10.2514/2.477
Reference41 articles.
1. Surge and Rotating Stall in Axial Flow Compressors—Part I: Theoretical Compression System Model
2. A Theory of Post-Stall Transients in Axial Compression Systems: Part I—Development of Equations
3. Vibration of Cascade Blades Treated by Actuator Disc Methods
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