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| author |   B. Watson <yalhcru@gmail.com> | 2022-03-12 14:41:26 -0500 |
|---|---|---|
| committer | B. Watson <yalhcru@gmail.com> | 2022-03-12 14:41:26 -0500 |
| commit | 39d0d102c6787abd9328d9b28cdf1bd72435f0d1 (patch) | |
| tree | 72e665f0ddd72c1590557e939ddc935dbbb23406 /academic | |
| parent | b4ebaf2b0015b98b285fddf74249c641d2a764aa (diff) | |
| download | slackbuilds-39d0d102c6787abd9328d9b28cdf1bd72435f0d1.tar.gz slackbuilds-39d0d102c6787abd9328d9b28cdf1bd72435f0d1.tar.xz | |
academic/xflr5: Wrap README at 72 columns.
Signed-off-by: B. Watson <yalhcru@gmail.com>
Diffstat (limited to 'academic')
| -rw-r--r-- | academic/xflr5/README | 8 |
1 files changed, 4 insertions, 4 deletions
diff --git a/academic/xflr5/README b/academic/xflr5/README index 1521ecb74b..628905a5a5 100644 --- a/academic/xflr5/README +++ b/academic/xflr5/README @@ -1,6 +1,6 @@ -XFLR5 is an analysis tool for airfoils, wings, and planes operating at low -Reynolds numbers. It includes: +XFLR5 is an analysis tool for airfoils, wings, and planes operating at +low Reynolds numbers. It includes: 1. XFoil's Direct and Inverse analysis capabilities -2. Wing design and analysis capabilities based on Lifting Line Theory, on the - Vortex Lattice Method, and on a 3D Panel Method +2. Wing design and analysis capabilities based on Lifting Line Theory, + on the Vortex Lattice Method, and on a 3D Panel Method |