Update summary:

• Span-efficiency factor (aka Oswald factor) included in results (and available as objective for optimizations)
• Drag-and-Drop: Aeolus ASP model files (*.xml) and CAD files (*.stp, *.obj, *.x3d) can be easily loaded through drag and drop
• New result charts of Center-of-pressure and Aerodynamic-center locations
• New result chart Cmy(Cl)
• Results include figures on the required power and thrust for level flight at different speeds
• Airfoil drop-down list is now searchable
• Lift distribution plot: added the elliptical reference curve
• New line force distribution view in 3d shows the strip-wise force components
• Optimization-, and Parameter-study progress panels are now equipped with chart controls to zoom in/out
• Improved the force balance 3d view
• CAD Model import transformations sequence improved and text fields aligned with this new sequence to make it more intuitive
• Aircraft reference surface changed to the sum of the reference surfaces of all wings in the model. Same with MAC, taken as the surface-weighted average.
• Fixed the sign of Cdi in the span-wise distribution charts. Now, local strip-wise thrust is shown as negative Cdi
• Password reset feature available in the sign-in panel
• As usual: bug fixes and performance improvements