🎉 Version 4.1 🎉

This is a functional release extending version 4.0 ...

Show laminar separation bubbles

• Based on Xfoil panel negative shear stress
• Visualized in in xtrt/xtrb polar

Scale reference airfoils and their polars

• Used to design airfoils along the wing sections
• Reynolds number of polars based on scale value

More...

• A lot of minor improvements and helper functions
• Bug fixes and refactorings

Please see README for more information

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Changelog

v 4.0 Major Release

• Setting Flap

  • Create 'flapped' airfoil as a design in Modify mode
  • Alternatively use 'flapped' polars for ad hoc analysis and comparisons

• Airfoil Optimzation

  • Uses Xoptfoil2 as optimization engine
  • Setup optimzation case with graphical operating point definition
  • Run and analyse an optimization case
  • Linux: workerand xoptfoil2have to be installed separately

• Simplified installation

  • Now available as Python package: pip install airfoileditor
  • Windows: Ready-built app as attached asset