MADO

pol

Multidisciplinary Aircraft Design Optimization

MADOflow_medium

These is framework for automated multidisciplinary aircraft optimization. Currently it includes such scientific disciplines as: aerodynamic analysis, strength analysis and dynamic stability analysis. Modular structure enables to include in the future other research fields. Main attention is focused on automation and data exchange processes. That is why we made available API for preparation of parametrized geometry, used in Panukl software for aerodynamic analysis. Panukl contains numerical tool for automated aerodynamic data preparation for SDSA – Simulation & Dynamic Stability Analysis. The geometry and aerodynamic load can be also exported to CalculiX software for strength analysis.

Documentation of input/output and configuration library for PANUKL and SDSA packages Config_API

Examples

MADO-MOSUPS_example

BoxWing optimization

FEMopt_medium

BoxWing - strength optimization

MADO-MOSUPS_medium

BoxWing - aerodynamic optimization

Stability

BoxWing - stability constraints