• AirCONICS (Python/Rhinoceros) download
  • Aircraft Geometry Toolbox (Matlab)
  • Chapter 2: Geometry parameterization – philosophy and practice
  • Chapter 3: Curves
  • Chapter 4: Surfaces
  • Chapter 5: Aerofoil Engineering – Fundamentals
  • Chapter 6: Families of Legacy Aerofoils
  • Chapter 7: Aerofoil Parameterization
  • Chapter 8: Planform Parameterization
  • Chapter 9: Three-Dimensional Wing Synthesis
  • Chapter_10: Design Sensitivities
  • Chapter_11: Basic Aerofoil Analysis: A Worked Example
  • Chapter_12: Human-Powered Aircraft Wing Design: A Case Study in Aerodynamic Shape Optimization
  • An AirCONICS-based unmanned air vehicle model
  • Terms & Conditions

Aircraft Geometry Codes

~ Parametric Models for Optimization, scripted in Python, Rhino and Matlab

Monthly Archives: October 2014

AirCONICS (Aircraft CONfiguration through Integrated Cross-disciplinary Scripting)

03 Friday Oct 2014

Posted by András Sóbester in Uncategorized

≈ Leave a comment

Screenshot 2014-10-03 20.34.09 AirCONICS is a free collection of parametric geometries defined as Rhinoceros/Python objects and scripts. They use the OpenNURBS framework through Rhinoceros and they can be run (using the RunPythonScript command) in Rhinoceros. The MacOS X version of Rhinoceros is available for free, while a trial version is available for free under Windows (the latter also features a neat IDE for developing Python code). The fundamental principle behind AirCONICS is that conceptual and preliminary design geometries can be defined (and stored) as scripts. This allows for:

  • easy parameterization of the geometry – all the variables of the code (including function handles) can be considered as potential parameters of the geometry
  • portability
  • the integration of complex design algorithms into the geometry – these can simply be part of the parametric ‘recipe’ that builds the geometry

You can get started with AirCONICS by downloading it here.

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Codes, etc.

  • AirCONICS (Python/Rhinoceros) download
  • Aircraft Geometry Toolbox (Matlab)
  • An AirCONICS-based unmanned air vehicle model
  • Chapter 2: Geometry parameterization – philosophy and practice
  • Chapter 3: Curves
  • Chapter 4: Surfaces
  • Chapter 5: Aerofoil Engineering – Fundamentals
  • Chapter 6: Families of Legacy Aerofoils
  • Chapter 7: Aerofoil Parameterization
  • Chapter 8: Planform Parameterization
  • Chapter 9: Three-Dimensional Wing Synthesis
  • Chapter_10: Design Sensitivities
  • Chapter_11: Basic Aerofoil Analysis: A Worked Example
  • Chapter_12: Human-Powered Aircraft Wing Design: A Case Study in Aerodynamic Shape Optimization
  • Errata
  • Terms & Conditions
  • UAV design book

Recent Posts

  • ADRpy – Aircraft Design Recipes in Python
  • Small Unmanned Fixed-Wing Aircraft Design
  • Wing sizing via constraint analysis
  • Standalone AirCONICS for Python
  • Design Optimization tools – some completely biased suggestions

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