A Mode Tracking Method in Aeroelastic Stability Analysis Using Left Eigenvectors

Author:

Hang Xiaochen1,Fei Qingguo1,Su Weihua2

Affiliation:

1. Southeast University

2. University of Alabama, Tuscaloosa

Publisher

American Institute of Aeronautics and Astronautics

Reference17 articles.

1. An Automated Procedure for Computing Flutter Eigenvalues

2. Use of eigenvectors in the solution of the flutter equation

3. New mode tracking methods in aeroelastic analysis

4. Gibson, W. C. “ASTROS-ID: Software for System Identification Using Mathematical Programming,” Tech. Rep. ADA260867, CSA Engineering Inc,Palo Alto CA, United States, 1992.

5. Damping Perturbation Method for Flutter Solution: The g-Method

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