airfoilplotter 0.0.1

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

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")