v2.0.1

What's Changed

• Fix sharpenTE/bluntTE making blunt TE on wrong condition by @akleb in #56
• Update .readthedocs.yaml by @eirikurj in #57
• NACA trailing edge fix by @sseraj in #58
• Added hyperbolic tangent distribution by @sseraj in #59
• Update package requirements by @marcomangano in #60

New Contributors

• @eirikurj made their first contribution in #57
• @sseraj made their first contribution in #58

Full Changelog: v2.0.0...v2.0.1

v2.0.0

New Features

• NACA 4-digit Airfoil by @akleb in #49
• Add option for LMS and Change Default Spline Order by @akleb in #50

Bug fixes

• Switching Max Camber to be in Airfoil Coordinates by @akleb in #39
• Update trailing edge modification to consistent format by @akleb in #42

Maintenance

• Adding More Tests by @akleb in #38
• splineUpdate by @Xiaosong2105 in #41
• Rename to prefoil by @akleb in #46
• Update azure-pipelines.yaml by @marcomangano in #52
• Docstrings and inconsistencies fix by @marcomangano in #51

Full Changelog: v1.2.0...v2.0.0

v1.2.0

This release adds camber line functionality.

Features

• Added camber line and thickness splines to the Airfoil class #36
• Plot function can now plot the camber line with an option
• Can compute the minimum and maximum camber Airfoil.getMaxCamber/Airfoil.getMinCamber
• Can check if an airfoil is symmetric Airfoil.isSymmetric
• Can compute the maximum thickness Airfoil.getMaxThickness
• Can now have Airfoil.getSampledPts add extra sampled points at the corner of a blunt trailing edge to indicate a knot in the spline #35
• Airfoil.getCTDistribution was renamed to Airfoil.getCDistribution and now it only returns camber points. A new function called Airfoil.getThickness now computes thickness points.

Maintenance

• Airfoil.translate should actually work now

v1.1.0

Features

• Adding self.sampled_pts (#34) Note that the function getPts() has been renamed to getSplinePts().

Maintenance

• Documentation updates (#30, #33)

v1.0.0

This is the initial stable release of pyfoil.