Oscillatory Subsonic Piecewise Continuous Kernel Function Method
- 1 June 1977
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 14 (6) , 515-516
- https://doi.org/10.2514/3.58813
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- A Quasi-Vortex-Lattice Method in Thin Wing TheoryJournal of Aircraft, 1974
- An oscillatory kernel function method for lifting surfaces in mixed transonic flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1974
- A doublet-lattice method for calculating lift distributions on oscillating surfaces in subsonic flows.AIAA Journal, 1969
- Effect of gaps on the loading distribution of planar lifting surfaces.AIAA Journal, 1968