Version 4.21 released

In this update:

  • Command line/API: AeolusASP can be run from the command line. The User Manual provides more information.
  • Airfoil contour in Cp plots: 2D plots of chord-wise pressure coefficients are now normalized and show the airfoil contour at the current strip. Also, a data table was added to export the plot data to any other plotting tool (right-click in the table)
  • Froude model: Propeller results now also include the Froude model.
  • The Power-Speed-Coefficient is computed for Propellers and available for Optimization or Parameter studies
  • Minor bugfixes of the login and licence panel.