Explicit Kutta Condition for Unsteady Two-Dimensional High-Order Potential Boundary Element Method
Author:
Affiliation:
1. Universita di Palermo, 90128 Palermo, Italy
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.197
Reference13 articles.
1. Boundary Integral Equations in Aerodynamics
2. Analysis of two-dimensional incompressible flows by a subsurface panel method
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4. Effect of airfoil (trailing-edge) thickness on the numerical solution of panel methods based on the Dirichlet boundary condition
5. Progress on the boundary element method to study the disturbance fields of bodies moving in an unbounded medium
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