Broadening interest by the aeronautics community in distributed electric propulsion systems has revealed a need for design and analysis methods capable of resolving the two-way coupling of aeropropulsive systems. A 2D, inviscid, and incompressible scheme to investigate the performance of these systems is described, which builds on prior, extensively used developments toward modeling airfoils in potential flow. The scheme incorporates a vortex panel method for multiple lifting geometries and iter