Coupled Bending-Torsion Flutter in a Supersonic Cascade
Author:
Affiliation:
1. University of Southern California, Los Angeles, Calif.
2. University of California, Los Angeles, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.51002
Reference22 articles.
1. Coupled Bending-Torsion Flutter in Cascades
2. 3Verdon, J. M. and McCune, J. E. "Unsteady Supersonic Cascade in Subsonic Axial Flow,'M//L4 Journal, Vol.13, Feb. 1975, pp.193-201.
3. Further Developments in the Aerodynamic Analysis of Unsteady Supersonic Cascades—Part 1: The Unsteady Pressure Field
4. On the Unsteady Supersonic Cascade With a Subsonic Leading Edge—An Exact First Order Theory—Part 1
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