File xflr5.changes of Package xflr5
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Wed Dec 26 08:15:10 UTC 2012 - dmitry_r@opensuse.org
- Update to version 6.09
* see included ReleaseNotes.txt for details
- spec file cleanup
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Tue Jun 26 00:00:00 UTC 2012 - adeperrois@xflr5.com
- xflr5 v6.07
* fixed type 2 batch polar analysis
* fixed the issue with incorrect 3D-panel calculations
* Corrected the incorrect aileron control derivatives
* Corrected the bug in wing analysis with ground effect
* Corrected the bug in type 4 analysis for wings and planes
* Corrected the bug which modified the chord length as twist increases:
impact results for wings with high dihedral
* Cleaned, corrected, and improved the code for B-Splines
* Removed the option for Min/Max type controls in Stabillity Polars
* Added an option to edit Wing Polar paramaters
* Fixed the crash bug when defining wings with more than 16 span sections
* Corrected a bug leading to incorrect results in stability derivatives
with active controls (CPanel::RotateBC())
* Removed the Splined Points Foil option
* Other minor corrections and enhancements
* Code cleaning
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Fri Jan 06 00:00:00 UTC 2012 - adeperrois@xflr5.com
- xflr5 v6.06
* Minor corrections and improvements
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Sun Jul 24 00:00:00 UTC 2011 - adeperrois@xflr5.com
- xflr5 v6.05 beta, July 15th, 2011
* For Type 7 polars, listed the control value instead of the aoa in the top drop down box
* Added a calculation form to determine Re.sqrt(Cl) for foil Type 2 polars
* Added the Japanese translation to the repository - thanks to Koichi
* Minor corrections and improvements
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Sun May 15 00:00:00 UTC 2011 - adeperrois@xflr5.com
- xflr5 v6.04 beta, May 14th, 2011
* added a settings save at each project save
* added and option to view forces on panels as coloured arrows
* fixed the incorrect setting of AVL-type controls for flaps in T7 analysis
* added the missing write operation in the project file of the control variable for wing operating points
* modified the setting of boundary conditions in T7 analysis with activated controls - impact on balanced aoa
* modified the wing construction process to allow for a gap in the middle of the wing
* corrected the bug which caused the disapperance of the left stability toolbar when switching to 3D view
* corrected the bug which prevented from changing the default number of panels in naca foil generation
* continued the code cleaning process
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Sun Feb 13 00:00:00 UTC 2011 - adeperrois@xflr5.com
- XFLR5v6.03 beta rpm release
* modified the geometry connection between panels with dihedral and twist - may slightly impact the results
* corrected the calculations with sideslip
* added multi-threading capability for foil batch analysis
* added an option to display the position of point masses in 3d-view
* in the export to AVL of point masses, corrected the missing addition of wing x & z position
* modified the export format to AVL of with wing flaps
* added an option to highlight the currently selected operating point, or the mode in root locs view
* changed the interface for stability analysis
* added a properties dialog box option for operating points
* corrected various minor bugs
* made several minor enhancements
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Sun Dec 19 00:00:00 UTC 2010 - adeperrois@xflr5.com
- XFLR5v6.02 beta rpm release
* added an option to load a background image in the foil direct design module
* corrected some errors in CoG and inertia automatic calculations, with impact on results
* did some deep code cleaning
* re-organized the panel analysis code to perform only one far field calculation per operating point
* optimized the panel method for increased speed of execution
* corrected the mesh edition for NURBS bodies
* changed the export format for graphs
* implemented the stability method for mixed panel/vlm method
* implemented the stability method for full 3D panel method
* corrected the bug which lead to incorrect results in 3D panel with Neumann B.C.
* corrected the error in the jump in potential at the wing's trailing edage in full 3d panel method
* set the estimation of inertia properties at the time of polar definition instead of evaluating at the time of analysis
* fixed the bug which could cause a crash when dragging a point in splines design
* corrected the asymetric transition location for symetric wings
* corrected the source strength influence of thick panels on thin surfaces, with impact on results for planes with body
* corrected the Cp 3D color display for VLM2 analysis
* added the influence of pressure forces acting on the body to induced pitching moment coefficient
* added calculation of neutral point position based on Cma/Cza ratio
* corrected various minor bugs
* made several minor enhancements
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Thu Oct 14 00:00:00 UTC 2010 - adeperrois@xflr5.com
- XFLR5v6.01 beta rpm release
* Corrected the incorrect balance speed in 3D type 2 polars for planes
* Corrected the final moment calculation in stability analysis
* Corrected the incorrect lift calculation in stability analysis
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Sat Sep 19 00:00:00 UTC 2010 - adeperrois@xflr5.com
- XFLR5v6.00 beta rpm release
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Fri Apr 3 00:00:00 UTC 2010 - adeperrois@xflr5.com
- First rpm release
