Pter0dacty is a programmed version of the NACA Technical Report 572 to determinate the characteristics of tapered wings.

Features

  • Accepts any geometrical planform
  • Selects and calculates the aditional and total lift coefficients
  • Generates the local lift distribution
  • Generates the lift, drag and polar curves
  • Accepts geometrical twisting
  • It's a MATLAB code
  • Next releases will include 3D wing plotting
  • Next releases will include aerodynamical twisting

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Registered

2017-12-15