hfoil: Hess-Smith panel code for inviscid 2-d airfoil analysis

[ bsd3, library, numerical, science ] [ Propose Tags ]

Library and command line REPL with plotting to do simple inviscid hess-smith panel code.

Features include:

  • Cheap and shameless xfoil ripoff for relp/plotting interface

  • Naca 4-series support with Gauss-Newton paneling

  • Broken UIUC database integration (type "uiuc [foilname]")

  • Haskeline interface with tab-completion (oooh)

  • Single and multi-element airfoils

  • Inviscid, incompressible, 2-dimensional flow only

To get started, do cabal install or whatever, then run the "hfoil" binary.

Things to try: "naca 2412", "alfa 4", (hit enter before entering another airfoil), "load [filename]", "uiuc e330"


Automatic Flags

Build the command line interface


Use -f <flag> to enable a flag, or -f -<flag> to disable that flag. More info


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Versions [RSS] 0.1.1, 0.1.2, 0.2.0,,
Dependencies base (>=4 && <5), directory (>=1.1), haskeline (>=0.6), hfoil (>=0.1.2), hmatrix (>=0.12), HTTP (>=4000.2), linear, not-gloss (>=, parsec (>=3.1.6), transformers (>=0.2) [details]
License BSD-3-Clause
Copyright (c) Greg Horn 2012, 2015
Author Greg Horn
Maintainer gregmainland@gmail.com
Category Numerical, Science
Source repo head: git clone git://github.com/ghorn/hfoil.git(tag 0.1.2)
Uploaded by GregHorn at 2015-05-23T19:57:05Z
Reverse Dependencies 1 direct, 0 indirect [details]
Executables hfoil
Downloads 3521 total (11 in the last 30 days)
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Status Docs available [build log]
Last success reported on 2015-05-25 [all 1 reports]