Evaluation of classical flutter analysis for the prediction of limit cycle oscillations
- 7 April 1997
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- A semi-empirical unsteady nonlinear aerodynamic model to predict transonic LCO characteristics of fighter aircraftPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1995
- A doublet-lattice method for calculating lift distributions on oscillating surfaces in subsonic flows.AIAA Journal, 1969