Udemy - Airfoil & Wing Aerodynamics, Design & Simulation with Python

Files Included :
1 1-1 Learning Objectives (30.89 MB)
10 1-10 Thickness Distribution (60.02 MB)
11 1-11 Calculating Thickness with PYTHON (65.2 MB)
12 1-12 Use non-dimensional values (122.38 MB)
13 1-13 Finding the Leading Edge Radius (99.74 MB)
14 1-14 Draw NACA 0018 with PYTHON (310.9 MB)
15 1-15 Draw NACA 2412 with PYTHON (400.51 MB)
16 1-16 Make NACA Airfoil Generator with Streamlit (399.99 MB)
17 1-17 Download Airfoil Data as CSV file (279.72 MB)
2 1-2 The Four Forces of Flight (52.89 MB)
3 1-3 Definition and Importance of Airfoils (63.01 MB)
4 1-4 Two Main Types Of Airfoils (71.32 MB)
5 1-5 Key Parameters of Airfoil (120.77 MB)
6 1-6 NACA Airfoil Classification (213.29 MB)
7 1-7 Geometric Construction (254.65 MB)
8 1-8 Calculating the Slope of the Camber Line (297.42 MB)
9 1-9 Calculating the Slope of the Camber Line with PYTHON (215.19 MB)

Screenshot
[Image: LTv13V5w_o.jpg]