Changelog for xflr5-6.08-85.1.x86_64.rpm :
Sat Oct 20 14:00:00 2012 A. Deperrois
- corrected the scaling of foil thickness and camber
- corrected the incorrect foil automatic polar name
- corrected the issue with zero-length wing sections
- corrected the occasional crash bug in plane definition with elevators
- minor bug corrections and enhancements

Tue Jun 26 14:00:00 2012 A. Deperrois
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

Fri Jan 6 13:00:00 2012 A. Deperrois
xflr5 v6.06
- Minor corrections and improvements

Sun Jul 24 14:00:00 2011 A. Deperrois
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

Sun May 15 14:00:00 2011 A. Deperrois
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

Sun Feb 13 13:00:00 2011 A. Deperrois
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

Sun Dec 19 13:00:00 2010 A. Deperrois
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

Thu Oct 14 14:00:00 2010 A. Deperrois
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

Sun Sep 19 14:00:00 2010 A. Deperrois
XFLR5v6.00 beta rpm release

Sat Apr 3 14:00:00 2010 A. Deperrois
First rpm release