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TUDuam documentation

  • Data Structures
  • Structures subpackage
  • Propulsion
  • Aerodynamics
  • Performance
    • Mass Metrics
    • Airfoil data generation
    • Propulsion Notebook
    • Structural Analysis
    • Structural Optimization
  • Data Structures
  • Structures subpackage
  • Propulsion
  • Aerodynamics
  • Performance
    • Mass Metrics
    • Airfoil data generation
    • Propulsion Notebook
    • Structural Analysis
    • Structural Optimization

Section Navigation

Contents:

  • Structural Optimization of a wingbox
  • Structural...

Structural Optimization#

Contents:

  • Structural Optimization of a wingbox
  • Laying out a framework for a full wing optimization
  • Constraining the design
    • Buckling
    • Von Mises failure Criterion
    • Other constraints
  • Leveraging Python for the optimization
  • Initialisation of parameters
  • Changing the amount of stringers
  • Example: Optimizing the wing of a Cessna 172R
    • Assumptions
  • Creating the section
  • Iterating over each section
  • Viewing the results

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Please run the code cell below to correctly initialize the notebook

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Structural Optimization of a wingbox

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