Damping Perturbation Method for Flutter Solution: The g-Method
Author:
Affiliation:
1. Zona Technology, Inc., Scottsdale, Arizona 85251
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.1171
Reference13 articles.
1. An approximate true damping solution of the flutter equation by determinant iteration.
2. A doublet-lattice method for calculating lift distributions on oscillating surfaces in subsonic flows.
3. A harmonic gradient method for unsteady supersonic flow calculations
4. Unsteady supersonic computations of arbitrary wing-body configurations including external stores
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