UNPA - Universal Parametric Geometry Representation Method

Version 1.0.0.0 (34.8 KB) by Massimiliano Di Muzio
Create analitically smooth airfoils
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Updated 24 May 2011

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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 .

MATLAB Release Compatibility
Created with R2010b
Compatible with any release
Platform Compatibility
Windows macOS Linux
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Version Published Release Notes
1.0.0.0