A tool for the design of Airfoils, Wings and Planes operating at low Reynolds numbers
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 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
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osc -A https://api.opensuse.org checkout openSUSE:Leap:42.3/xflr5 && cd $_
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Source Files
Filename | Size | Changed |
---|---|---|
xflr5-6.10.04_src.tar.gz | 0002537802 2.42 MB | |
xflr5.changes | 0000007943 7.76 KB | |
xflr5.desktop | 0000000546 546 Bytes | |
xflr5.spec | 0000002655 2.59 KB |
Revision 4 (latest revision is 5)
Ludwig Nussel (lnussel_factory)
committed
(revision 4)
branch from 42.2
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