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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