PANUKL 2024

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. All programs were changed and modernized. Details are included in Change Log file. Current version contains the option to export the geometry and the results (pressure distribution) to FEM analysis (Calculix)

Package contains new version of manual - some new chapters are coming soon.

Downloads:

PANUKL 2024 (2.2):

• MS Windows installation version combined 32/64 bit (updated: 2.09.2024, rev.1132)
• MS Windows installation version 32 bit (updated: 2.09.2024, rev.1132)
• MS Windows installation version 64 bit (updated: 2.09.2024, rev.1132)
• Linux installer 32 (updated: 14.02.2023, rev.1054)
• Linux binary version 32 (updated: 14.02.2023, rev.1054)
• Linux installer 64 (updated: 13.02.2023, rev.1054)
• Linux binary version 64 (updated: 13.02.2023, rev.1054)
• Config_API - documentation of input/output and configuration library for PANUKL and SDSA packages
• Config_LIB - source files of input/output and configuration library
• ANSYS Workbench Panukl extension - plugin for ANSYS software
• Packet changes description file

Sample data files (included in the installation version):

• Various wing versions
• "Predator" aircraft
• "TurboProp" aircraft
• Short comment on the samples

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:

• PANUKL 2020 User's Guide

With any suggestions/complaints please write to:

tgrab@meil.pw.edu.pl

including a word "PANUKL" in the message title.