Hello community, here is the log from the commit of package xflr5 for openSUSE:Factory checked in at 2012-12-28 22:51:14 ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ Comparing /work/SRC/openSUSE:Factory/xflr5 (Old) and /work/SRC/openSUSE:Factory/.xflr5.new (New) ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++
Package is "xflr5", Maintainer is "" Changes: -------- New Changes file: --- /dev/null 2012-12-21 01:49:00.356010756 +0100 +++ /work/SRC/openSUSE:Factory/.xflr5.new/xflr5.changes 2012-12-28 22:51:15.000000000 +0100 @@ -0,0 +1,115 @@ +------------------------------------------------------------------- +Wed Dec 26 08:15:10 UTC 2012 - [email protected] + +- Update to version 6.09 + * see included ReleaseNotes.txt for details +- spec file cleanup + +------------------------------------------------------------------- +Tue Jun 26 00:00:00 UTC 2012 - [email protected] + +- 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 06 00:00:00 UTC 2012 - [email protected] + +- xflr5 v6.06 + * Minor corrections and improvements + +------------------------------------------------------------------- +Sun Jul 24 00:00:00 UTC 2011 - [email protected] + +- 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 00:00:00 UTC 2011 - [email protected] + +- 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 00:00:00 UTC 2011 - [email protected] + +- 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 00:00:00 UTC 2010 - [email protected] + +- 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 00:00:00 UTC 2010 - [email protected] + +- 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 + +------------------------------------------------------------------- +Sat Sep 19 00:00:00 UTC 2010 - [email protected] + +- XFLR5v6.00 beta rpm release + +------------------------------------------------------------------- +Fri Apr 3 00:00:00 UTC 2010 - [email protected] + +- First rpm release New: ---- xflr5-6.09.tar.bz2 xflr5.changes xflr5.desktop xflr5.spec ++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++++ Other differences: ------------------ ++++++ xflr5.spec ++++++ # # spec file for package xflr5 # # Copyright (c) 2012 SUSE LINUX Products GmbH, Nuernberg, Germany. # # All modifications and additions to the file contributed by third parties # remain the property of their copyright owners, unless otherwise agreed # upon. The license for this file, and modifications and additions to the # file, is the same license as for the pristine package itself (unless the # license for the pristine package is not an Open Source License, in which # case the license is the MIT License). An "Open Source License" is a # license that conforms to the Open Source Definition (Version 1.9) # published by the Open Source Initiative. # Please submit bugfixes or comments via http://bugs.opensuse.org/ # Name: xflr5 Version: 6.09 Release: 0 License: GPL-2.0 Group: Productivity/Scientific/Other Summary: Analysis tool for airfoils and planes operating at low Re numbers URL: http://xflr5.com # there is no released tarballs # svn checkout svn://svn.code.sf.net/p/xflr5/code/branches/xflr5-%{version} xflr5-%{version} Source0: %{name}-%{version}.tar.bz2 Source1: %{name}.desktop BuildRequires: gcc-c++ BuildRequires: libqt4-devel >= 4.7.0 BuildRequires: Mesa-devel BuildRoot: %{_tmppath}/%{name}-%{version}-build %description XFLR5 is a design tool intended for the design and analysis of reduced scaled model airplanes. It includes the XFoil program for the analysis of airfoils. It includes a non-linear Lifting Line method (LLT), two Vortex Lattice Methods (VLM), and a 3D panel flat panel,first-order method for the analysis of wings and planes. XFLR5 v5 is a re-write of XFLR5 v4 using Qt4 libraries instead of Microsoft's MFC. XFLR5 v6 introduces stability and control analysis %prep %setup -q cp %{SOURCE1} . # fix wrong-file-end-of-line-encoding sed -i 's/\r$//' {License.txt,doc/ReleaseNotes.txt} %build qmake -o Makefile %{name}_%{version}.pro make %{?_smp_mflags} lrelease %{name}_%{version}.pro %install install -Dm 755 %{name} %{buildroot}%{_bindir}/%{name} install -Dm 644 images/%{name}.png %{buildroot}%{_datadir}/pixmaps/%{name}.png install -Dm 644 %{name}.desktop %{buildroot}%{_datadir}/applications/%{name}.desktop install -d %{buildroot}%{_datadir}/%{name}/translations install -m 644 translations/*.qm %{buildroot}%{_datadir}/%{name}/translations %files %defattr(-,root,root) %doc License.txt doc/ReleaseNotes.txt doc/*.odt %{_bindir}/%{name} %{_datadir}/%{name}/ %{_datadir}/applications/%{name}.desktop %{_datadir}/pixmaps/%{name}.png %changelog ++++++ xflr5.desktop ++++++ [Desktop Entry] Categories=Engineering; Comment[en_US]=XFLR5 is an analysis tool for airfoils, wings and planes operating at low Reynolds numbers Comment=XFLR5 is an analysis tool for airfoils, wings and planes operating at low Reynolds numbers Exec=xflr5 %u GenericName[en_US]=XFLR5 v6 GenericName=XFLR5 v6 Icon=xflr5 MimeType= Name[en_US]=xflr5 Name=xflr5 Path= StartupNotify=true Terminal=false TerminalOptions= Type=Application X-DBUS-ServiceName= X-DBUS-StartupType= X-KDE-SubstituteUID=false X-KDE-Username= X-SuSE-translate=true -- To unsubscribe, e-mail: [email protected] For additional commands, e-mail: [email protected]
