Airfoil & Wing Aerodynamics, Design & Simulation with Python
Python for Aerospace: Airfoil Design and Calculation of Lift, Drag, and Moment Coefficients
4.72 (9 reviews)
90
students
6 hours
content
Sep 2024
last update
$13.99
regular price
What you will learn
Grasp the fundamental forces acting on an aircraft.
Learn the significance and role of airfoils in aerodynamics.
Identify critical parameters that define airfoil performance.
Understand the NACA system for classifying airfoils.
Master the geometric principles behind airfoil design.
Learn to calculate the slope of the camber line analytically.
Implement Python programming to compute camber line slopes.
Analyze and calculate the thickness distribution of airfoils.
Understand the importance of non-dimensional analysis in aerodynamics.
Create graphical representations of the NACA 0018 airfoil using Python.
Generate visualizations for the NACA 2412 airfoil using Python.
Build an interactive airfoil generator application using Streamlit.
Learn how to export airfoil data in CSV format for analysis.
Understand and compute lift and drag forces acting on airfoils using Python.
Gain skills in simulating airfoil behavior and performance through Python programming.
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6121015
udemy ID
11/08/2024
course created date
21/08/2024
course indexed date
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