Novel Implementation of Hess and Smith panel method using Data structures

Version 1.1.0.0 (5.33 KB) by ronak gupta
Code to plot pressure variation on NACA 4 digit aerofoil and calculate lift variation
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Updated 20 Feb 2013

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This is a an implementation of Hess and Smith panel method. The program can plot pressure variation plots for 4 digit aerofoils and calculate coefficient of lift. It can be used for basic subsonic analysis. README file is included for input instructions

Cite As

ronak gupta (2026). Novel Implementation of Hess and Smith panel method using Data structures (https://www.mathworks.com/matlabcentral/fileexchange/39237-novel-implementation-of-hess-and-smith-panel-method-using-data-structures), MATLAB Central File Exchange. Retrieved .

MATLAB Release Compatibility
Created with R2010a
Compatible with any release
Platform Compatibility
Windows macOS Linux
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Version Published Release Notes
1.1.0.0

Update in title
1.0.0.0