Finite Wings
Author:
Publisher
John Wiley & Sons, Ltd
Reference35 articles.
1. A doublet-lattice method for calculating lift distributions on oscillating surfaces in subsonic flows;Albano;AIAA Journal,1969
2. Nonlinear aeroelastic formulation and postflutter analysis of flexible high-aspect-ratio wings;Arena;Journal of Aircraft,2013
3. A theoretical and experimental investigation of the effects of a steady angle of attack on the nonlinear flutter of a delta wing plate model;Attar;Journal of Fluids and Structures,2003
4. Cantilevered plate Rayleigh-Ritz trial function selection for von Kármán's plate equations;Attar;Journal of Aircraft,2007
5. Blair M 1994 A compilation of the mathematics leading to the doublet-lattice method
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