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Releases: chiefenne/PyAero

PyAero version 2.1.6

26 Dec 18:59
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New Contributors

Full Changelog: v2.1.5...v2.1.6

PyAero version 2.1.5

25 Feb 00:45
d9a8057
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Added smoothers and exposed them to the user. Only mesh block 3 is smoothed at the moment. Needs further improvement.
Many small additions and fixes.
Significant update of the documentation. Still a lot missing.

What's Changed

New Contributors

Full Changelog: v2.1.4...v2.1.5

PyAero version 2.1.4

04 Nov 07:45
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Fixed trailing edge meshing in batch mode

What's Changed

  • fixed trailing edge mesh in batch mode meshing by @chiefenne in #24

Full Changelog: v2.1.3...v2.1.4

PyAero version 2.1.3

03 Nov 20:00
ede43b1
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fixed boundary markers (tags) for SU2 mesh export

What's Changed

Full Changelog: v2.1.2...v2.1.3

PyAero version 2.1.2 fix

01 Nov 15:28
ca33b1c
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The main update concerns fixing the SU2 boundary definitions.

What's Changed

Full Changelog: v2.1.1...v2.1.2

PyAero version 2.1

28 Oct 07:46
d83925f
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Added the possibility to run PyAero in batch mode, i.e. run the meshing process from the command line.

What's Changed

Full Changelog: v2.0.2...v2.1.0

PyAero version 2.0.2

10 Oct 21:50
7ef45b7
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Corrected several bugs
Added mean camber line and camber and thickness calculation

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Full Changelog: v2.0.1...v2.0.2

PyAero version 2.0.1

17 Sep 16:11
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  • fixed writing several mesh formats
  • tests done for VTK, ABAQUS and AVL-FIRE
  • corrected version

Full Changelog: v2.0...v2.0.1

PyAero version 2.0

16 Sep 22:19
cc31580
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New release of PyAero

  • Moved from Pyside2 to Pyside6
  • Refactored and fixed connecting algorithm for mesh blocks
  • Added meshio library to allow multiple output formats
  • Fixed icon paths
  • Several other fixes

What's Changed

Full Changelog: v1.2...v2.0

PyAero version 1.2

05 Sep 18:07
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This version has some updates specifically for the mesh export in SU2 and GMSH formats. It includes the definition of boundary conditions for airfoil, outer boundary and symmetry. Still some updates are planned here.

An initial implementation of a geometrical airfoil contour analysis was added.