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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:

  • Preliminary sizing of a rotor blade
  • Propulsion Notebook

Propulsion Notebook#

Contents:

  • Preliminary sizing of a rotor blade
    • Defining the conditions
  • Running the optimisation
  • Offdesign analysis
  • Hover example
    • Sources
  • Finding the max thrust of a blade
  • Iteration of the rotor design.

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Creating airfoil data for various Reynolds numbers

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Preliminary sizing of a rotor blade

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