@hackage / hfoil

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

Latest0.2.0.2

About

Metadata

  • Last updated , by GregHorn
  • License BSD-3-Clause
  • Categories Mathematics

  • Maintained by: gregmainland@gmail.com

  • Lottery factor: 0

Links

Installation

Package Flags

Use the -f option with cabal commands to enable flags

    repl (on by default)

    Build the command line interface

Readme

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"