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 7
|
Lecture 7 - Elliptical Lift Distribution
Elliptical Lift Distribution
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
To view the lecture material accompanying this lecture in a new window, please click the button below. If necessary, use the vertical or horizontal scrollbar in the new window to view more of the material or you can resize the window.
To download the above lecture material use this link. (Right-click and select Save Target As or Save Link As.)
Supplementary lecture material is listed below.1. Student Questions
2. Assignment F7
3. Assignment F7 Solution
