airfoil

Version 2.0.0 (125 Bytes) by D KUSHAL KUMAR
Plot your own 4-digit airfoil by entering your maximum chamber and thickness.
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Updated 5 Jul 2019
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Using the standard formula and experimental value. This code will plot the airfoil as per the User input and further can save in image format.

Cite As

D KUSHAL KUMAR (2024). airfoil (https://github.com/VENA009/airfoil), GitHub. Retrieved .

MATLAB Release Compatibility
Created with R2018b
Compatible with R2007b and later releases
Platform Compatibility
Windows macOS Linux
Categories
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Version Published Release Notes
2.0.0

plot your own airfoil.
1.0.0

To view or report issues in this GitHub add-on, visit the GitHub Repository.
To view or report issues in this GitHub add-on, visit the GitHub Repository.