A Quasi-Vortex-Lattice Method in Thin Wing Theory
- 1 September 1974
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 11 (9) , 518-527
- https://doi.org/10.2514/3.60381
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- Remarks on vortex-lattice methods.Journal of Aircraft, 1973
- Leading-edge force features of the aerodynamic finite element method.Journal of Aircraft, 1972
- Comment on " Span wise Distribution of Induced Drag in Subsonic Flow by the Vortex Lattice Method"Journal of Aircraft, 1971
- Spanwise distribution of induced drag in subsonic flow by the vortexlattice methodJournal of Aircraft, 1970
- On the singularity method of subsonic lifting- surface theoryJournal of Aircraft, 1969
- The Lift on a Thin Aerofoil with a Jet-Augmented FlapAeronautical Quarterly, 1958