• Airframe geometry files are completely internally generated, requiring no outside CAD tools
• The module workflow is inspired by industry standard drafting techniques, and is specialized so that wing-type and fuselage-type shapes can be defined much easier than using general CAD software
• An airframe can have any number of freely positioned wing and fuselage objects, enabling creation of wide varieties of unorthodox and original aircraft configurations

• The mesher converts the airframe geometry into a form suitable for solving the flow equations
• The airframe is approximated as a polygonal mesh; a closed surface consisting of triangles and quadrilaterals
• The user does not need to explicitly name connected bodies; if any two bodies intersect, the mesher will automatically patch them together into a single closed waterproof surface
• Complex shapes can be created by defining multiple bodies and positioning them so that they intersect

The flow solver in this toolset offers a robust selection of panel element types, providing users with the flexibility to model aerodynamic flows with varying levels of fidelity. It includes constant and linear source panels, ideal for potential flow modeling and understanding basic aerodynamic interactions. Additionally, vortex line elements allow for efficient wake modeling and lift calculations, making them particularly useful for wing and lifting surface analysis. For more advanced simulations, the solver incorporates linear and quadratic doublet panels, enabling higher accuracy in representing complex surface curvature and flow interactions. This comprehensive range of panel methods ensures that both students and professionals can tailor their analyses to suit anything from introductory aerodynamic studies to high-fidelity aircraft design and optimization.