On the use of Pade approximants to represent unsteady aerodynamic loads for arbitrarily small motions of wings
- 26 January 1976
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Potential flow about three-dimensional lifting configurations, with application to wings and rotorsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1975
- A doublet-lattice method for calculating lift distributions on oscillating surfaces in subsonic flows.AIAA Journal, 1969
- LetterJournal of the Aeronautical Sciences, 1941