Development of an advanced panel method for complex configurations in subsonic compressible flow; Application to the computation of the potential flow through ducts.

The application of a boundary integral or "panel" method to duct flows is described. The method is capable of computing the three dimensional, steady state, subsonic, linearized (Prandtl-Glauert) potential flow about general configurations. The method is characterized by the application of a Dirichlet boundary condition and of "compressible"...