Novel Implementation of Hess and Smith panel method using Data structures
Code to plot pressure variation on NACA 4 digit aerofoil and calculate lift variation
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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 .
General Information
- Version 1.1.0.0 (5.33 KB)
MATLAB Release Compatibility
- Compatible with any release
Platform Compatibility
- Windows
- macOS
- Linux
