Vortex-Lattice Method for the Calculation of the Nonsteady Separated Flow over Delta Wings
- 1 December 1981
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 18 (12) , 1032-1037
- https://doi.org/10.2514/3.57596
Abstract
No abstract availableKeywords
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- A numerical method for the calculation of nonlinear, unsteady lifting potential flow problemsAIAA Journal, 1969