Pter0dactyl

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

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