airfoil
Plot your own 4-digit airfoil by entering your maximum chamber and thickness.
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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 (2026). airfoil (https://github.com/VENA009/airfoil), GitHub. Retrieved .
General Information
- Version 2.0.0 (125 Bytes)
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View License on GitHub
MATLAB Release Compatibility
- Compatible with R2007b and later releases
Platform Compatibility
- Windows
- macOS
- Linux
Versions that use the GitHub default branch cannot be downloaded
| Version | Published | Release Notes | Action |
|---|---|---|---|
| 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.
