| 1 - Introduction.mp4 | 26.5 MB | ||
| 2 - 1 Overview of CST Method.mp4 | 95.3 MB | ||
| 3 - 2 Use CST Method with Python.mp4 | 146 MB | ||
| 4 - 3 Understanding of Bernstein Polynomial.mp4 | 198.3 MB | ||
| 5 - 4 Understanding of the Effect of the Number of Coefficients.mp4 | 204 MB | ||
| 6 - 5 Effect of the values of N1 and N2.mp4 | 83.3 MB | ||
| 7 - 6 Visualization of the Airfoil.mp4 | 101 MB | ||
| Bonus Resources.txt | 409.6 B | ||
| Get Bonus Downloads Here.url | 204.8 B |
Mastering Airfoil Optimization: From Design To Performance
https://FreeCourseWeb.com
Published 1/2025
MP4 | Video: h264, 1920x1080 | Audio: AAC, 44.1 KHz
Language: English | Size: 854.37 MB | Duration: 1h 33m
Design with CST, Analyze with XFOIL, and Optimize with Deep Reinforcement Learning
What you'll learn
Understanding airfoil shapes and their significance in aerodynamics.
How to implement the Class Shape Transformation (CST) method.
Creating and manipulating airfoil shapes using CST parameters.
Using Python libraries (e.g., NumPy, Matplotlib) for airfoil design and visualization.
Writing Python code to implement the CST method.
Setting up and executing XFOIL simulations to analyze airfoil performance.
Extracting lift and drag coefficients from XFOIL results.
Understanding how to interpret lift and drag data.
Analyzing the impact of airfoil shape on aerodynamic performance.
Basics of reinforcement learning and its application in optimization problems.
Implementing DRL algorithms to optimize airfoil shapes for improved performance.
Evaluating the effectiveness of optimized designs through simulations.
Case studies nstrating successful airfoil design and optimization.
Hands-on projects that involve designing, analyzing, and optimizing airfoils using the techniques learned.
Requirements
Basic Mathematics: Understanding of algebra, geometry, and calculus.
Python Programming: Familiarity with Python programming, including libraries such as NumPy and Matplotlib.
Fundamentals of Aerodynamics: Basic knowledge of aerodynamic principles, including lift, drag, and airfoil characteristics.
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