UNPA - Universal Parametric Geometry Representation Method
The purpose of this code is to create analitically smooth airfoils starting from user supplied airfoils.
Airfoils can be supplied either Clockwise or Counter Clockwise. Geometrical shape class managed: NACA-type airfoil,Elliptic airfoil,Biconvex airfoil, Sears-Haack distribution,Projectile,Wedge,Circular duct.
Cite As
Massimiliano Di Muzio (2024). UNPA - Universal Parametric Geometry Representation Method (https://www.mathworks.com/matlabcentral/fileexchange/31544-unpa-universal-parametric-geometry-representation-method), MATLAB Central File Exchange. Retrieved .
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Version | Published | Release Notes | |
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1.0.0.0 |