Role of shocks in transonic/supersonic compressor rotor flutter
Author:
Affiliation:
1. Princeton University, Princeton, New Jersey
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.9411
Reference24 articles.
1. On the Unsteady Supersonic Cascade With a Subsonic Leading Edge—An Exact First Order Theory—Part 1
2. Unsteady Supersonic Cascade in Subsonic Axial Flow
3. Unsteady Flow in a Supersonic Cascade with Subsonic Leading-Edge Locus
4. Coupled Bending-Torsion Flutter in a Supersonic Cascade
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