a package for the computation of nonlinear lifting line for wings for Octave.
This package allows efficient computation of nonlinear aerodynamic properties of a wing. It employs 2D section data to build a 3D potential vortex model of the flow. It uses a robust Euler-Newton method to track the change of flow vorticity quantities as the angle of attack progresses.
released on 2 March 2009
- Octave-ad Octave-ann Octave-audio Octave-benchmarks Octave-bim Octave-bioinfo Octave-cdf Octave-civilengineering Octave-combinatorics Octave-communications Octave-control Octave-data smoothing Octave-db Octave-econometrics Octave-engine Octave-financial Octave-fixed Octave-fpl Octave-ga Octave-general Octave-generatehtml Octave-gpr Octave-graceplot Octave-gsl Octave-ident
Extension or PluginThis package can be used as an extension, plugin, or add-on to:
|License||Verified by||Verified on||Notes|
|License:GPLv3orlater||Kelly Hopkins||28 July 2009|
Leaders and contributors
Resources and communication
|Developer||VCS Repository Webview||https://sourceforge.net/p/octave/nlwing2/|
|Required to use||Octave >= 3.0.0|
This entry (in part or in whole) was last reviewed on 22 January 2017.
Permission is granted to copy, distribute and/or modify this document under the terms of the GNU Free Documentation License, Version 1.3 or any later version published by the Free Software Foundation; with no Invariant Sections, no Front-Cover Texts, and no Back-Cover Texts. A copy of the license is included in the page “GNU Free Documentation License”.
The copyright and license notices on this page only apply to the text on this page. Any software or copyright-licenses or other similar notices described in this text has its own copyright notice and license, which can usually be found in the distribution or license text itself.