Lectures
- 1. Formation of Lifting Flow
- 2. Airfoil Vortex Sheet Models
- 3. Thin Airfoil Analysis Problem (cont)
- 4. Thin Airfoil Theory Application
- 5. Introduction to 3D Wings
- 6. Lifting Line Theory
- 7. Elliptical Lift Distribution
- 8. Wing Design Problem
- 9. General Wings
- 10. Aircraft Performance Analysis
- 11. Introduction to Compressible Flows
- 12. Energy Conservation
- 13. Stagnation Quantities
- 14. Normal Shock Waves
- 15. Mach Number Relations
- 16. Shock Losses
- 17. Oblique Shocks
- 18. Shock Expansion Theory
- 19. Compressible Channel Flow
- 20. Laval Nozzle Flows
Fluid Mechanics II - Lecture 6
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Lecture 6 - Lifting Line Theory
3D Vortex Filaments, Lifting Line Theory
Prof. Mark Drela
16.03-16.04 Fluid Mechanics (Massachusetts Institute of Technology: MIT OpenCourseWare) http://ocw.mit.edu Date accessed: 2009-04-04 License: Creative Commons BY-NC-SA |
Lecture Material
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Supplementary lecture material is listed below.1. Student Questions
2. Assignment F6
3. Assignment F6 Solution
