Package to compute the aerodynamic characteristics of an aircraft using low order panel method.


The new version of PANUKL package contains a lot of significant changes, mainly in pre- and post-processing. Details are included in Change Log file. Current version contains new mesh generator and MS2Editor. The old version of mesh generator is still embedded (user can select mesh generator: Create->Select Mesh Generator). New geometry definition methods are available only in the new mesh generator. Current version contains also option to export the geometry and the results (pressure distribution) to FEM analysis (Calculix)

Package contains the old version of manual - new version is coming soon.


PANUKL 2012 package - current version:

Development version:

PANUKL 2002 package - archive version:

Sample data files (included in the installation version):

Full user's guide (included in the installation version)

PANUKL includes help system added to installation file, and available as an option in the packet program. the help system requires a PDF file browser.

Link to the full guide for people, who want to read it before installing the program, is shown below:

With any suggestions/complaints please write to:

including a word "PANUKL" in the message title.