A subsonic oscillating-surface theory for wings with partial-span controls
- 17 January 1972
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- A generalized quadrature formula for Cauchy integralsAIAA Journal, 1971
- A doublet-lattice method for calculating lift distributions on oscillating surfaces in subsonic flows.AIAA Journal, 1969
- Use of complex cross-flow representation in nonplanar oscillating-surface theory.AIAA Journal, 1968
- On the approximation of the normal velocity on oscillating wings.AIAA Journal, 1966