On Tracking Aeroelastic Modes in Stability Analysis Using Left and Right Eigenvectors
Author:
Affiliation:
1. Southeast University, Nanjing, Jiangsu 211189, People’s Republic of China
2. The University of Alabama, Tuscaloosa, Alabama 35487-0280
Funder
China Scholarship Council
University of Alabama
Scientific Research Innovation Program of Jiangsu Province College Postgraduates
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference27 articles.
1. FungY. C., An Introduction to the Theory of Aeroelasticity, Dover Publ., New York, 1993, pp. 377–379.
2. New mode tracking methods in aeroelastic analysis
3. An Automated Procedure for Computing Flutter Eigenvalues
4. Use of eigenvectors in the solution of the flutter equation
5. GibsonW. C. “ASTROS-ID: Software for System Identification Using Mathematical Programming,” CSA Engineering Inc. TR ADA260867, Palo Alto, CA, 1992.
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