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

Project Samples

Pter0dactyl Screenshot 1 Pter0dactyl Screenshot 2

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Additional Project Details

Registered

2017-12-15
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