A vortex-lattice method for general, unsteady aerodynamics
- 1 January 1985
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 22 (1) , 43-49
- https://doi.org/10.2514/3.45078
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
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- Vortex-Lattice Method for the Calculation of the Nonsteady Separated Flow over Delta WingsJournal of Aircraft, 1981
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- Nonlinear Prediction of Aerodynamic Loads on Lifting SurfacesJournal of Aircraft, 1976
- Extension of a Vortex-Lattice Method to Include the Effects ofLeading-Edge SeparationJournal of Aircraft, 1974
- Wing-Body Aerodynamic InteractionAnnual Review of Fluid Mechanics, 1972