@hackage hfoil0.2.0.2

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

Categories
- Mathematics
License
BSD-3-Clause
Maintainer
gregmainland@gmail.com
Links
Versions
- 0.2.0.2 Sat, 23 May 2015
- 0.2.0.1 Sun, 15 Mar 2015
- 0.2.0 Sat, 14 Mar 2015
- 0.1.2 Fri, 10 Feb 2012
- 0.1.1 Thu, 9 Feb 2012

Installation
In your cabal file:
Dependencies (9)
- base >=4 && <5
- hfoil >=0.1.2
Dependents (1)
@hackage/acme-everything

Package Flags

repl

(on by default)

Build the command line interface

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"