New mode tracking methods in aeroelastic analysis
Author:
Affiliation:
1. University of Michigan, Ann Arbor, Michigan 48109
2. U.S. Air Force Flight Dynamics Directorate, Wright-Patterson Air Force Base, Ohio 45433
3. University of Michigan, Ann Arbor, Michigan 48109
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.12552
Reference17 articles.
1. 2Eldred, M. S. "Full Order Eigenpair Perturbations with Mode Tracking Applications in Aeroelasticity and Optimization," Ph.D. Dissertation,Univ. of Michigan, Ann Arbor, MI, 1993.
2. An Automated Procedure for Computing Flutter Eigenvalues
3. Use of eigenvectors in the solution of the flutter equation
4. Higher order eigenpair perturbations
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