Metadata-Version: 2.4
Name: airfoilplotter
Version: 0.0.1
Summary: A Python library for generating and plotting NACA airfoils (4-, 5-, 6-, and 7-series).
Author: Amandeep Singh, Tuiba Ashraf
Author-email: amandeepoct97@gmail.com, tuiba.ashraf107@gmail.com
License: MIT
Classifier: Programming Language :: Python :: 3
Classifier: License :: OSI Approved :: MIT License
Classifier: Operating System :: OS Independent
Classifier: Intended Audience :: Science/Research
Classifier: Topic :: Scientific/Engineering :: Physics
Requires-Python: >=3.8
Description-Content-Type: text/markdown
License-File: LICENSE
Requires-Dist: numpy>=1.24.0
Requires-Dist: matplotlib>=3.7.0
Dynamic: author
Dynamic: author-email
Dynamic: classifier
Dynamic: description
Dynamic: description-content-type
Dynamic: license
Dynamic: license-file
Dynamic: requires-dist
Dynamic: requires-python
Dynamic: summary

# airfoilplotter

A Python library for generating and plotting NACA airfoils (4, 5, 6, and 7 series).

## ✈️ Features
- Generate NACA 4, 5, 6, and 7 series airfoil coordinates
- Plot airfoil shape with Matplotlib
- Lightweight and easy to use

## 📦 Installation

# How to Use Library

# Example 1: NACA 4-series

# Unsymmetric airfoil (NACA 2412)
from airfoilplotter import naca4, plot_airfoil
xu, yu, xl, yl = naca4(0.02, 0.4, 0.12, symmetric=False)
plot_airfoil(xu, yu, xl, yl, "NACA 2412 (Unsymmetric)")

# Symmetric airfoil (NACA 0012)
xu, yu, xl, yl = naca4(0, 0, 0.12, symmetric=True)
plot_airfoil(xu, yu, xl, yl, "NACA 0012 (Symmetric)")

# Example 2: NACA 5-series
from airfoilplotter import naca5, plot_airfoil
xu, yu, xl, yl = naca5(0.3, 0.4, 0.12)
plot_airfoil(xu, yu, xl, yl, "NACA 5-Series Airfoil")

# Example 3: NACA 6-series
from airfoilplotter import naca6, plot_airfoil
xu, yu, xl, yl = naca6(0.3, 0.12)
plot_airfoil(xu, yu, xl, yl, "NACA 6-Series Airfoil")

# Example 4: NACA 7-series
from airfoilplotter import naca7, plot_airfoil
xu, yu, xl, yl = naca7(0.3, 0.12)
plot_airfoil(xu, yu, xl, yl, "NACA 7-Series Airfoil")
