Fluid Mechanics and Aerodynamics
Professor Mark Drela
Spring
2006
|
Fluid Mechanics and Aerodynamics |
|
Spring
2006
|
|
Lecture
|
Date
|
Topic
|
Lecture Notes | Anderson, Third Edition |
| F1 |
2/7
|
Formation of Lifting Flow
|
4.5, 4.6 | |
| F2 |
2/8
|
Airfoil Vortex Sheet Models, Thin Airfoil Analysis Problem
|
4.4, 4.7 | |
| F3 |
2/10
|
Thin Airfoil Analysis Problem, Continued
|
4.8 | |
| F4 |
2/13
|
Thin Airfoil Theory Application: Analysis Example
|
4.8, 4.9 | |
| F5 |
2/14
|
Introduction to 3D Wings, 2D and 3D Coefficients
|
5.1 |
|
| F6 |
2/15
|
3D Vortex Filaments, Lifting Line Theory
|
5.1 | |
| F7 |
2/17
|
Elliptical Lift Distribution
|
5.3.1 | |
| F8 |
2/21
|
Wing Geometry, Wing Design Problem
|
5.3.2, 5.3.3 | |
| F9 |
2/22
|
General Wings
|
5.3.2, 5.3.3 | |
| F10 |
2/23
|
Aircraft Performance Analysis (updated Feb 22)
|
||
| F11 |
2/24
|
Intorduction to Compressible Flows, Thermodynamic Concepts
|
7.1-7.2
|
|
| F12 |
2/28
|
Energy Conservation
|
2.7, 7.4, 7.5 | |
| F13 |
3/6
|
Stagnation Quantities, Introduction to Shock Waves
|
7.5, 7.6 | |
| F14 |
3/7
|
Normal Shock Waves, Speed of Sound
|
8.1-8.3 | |
| F15 |
3/8
|
Mach Number Relations, Normal Shock Properties
|
8.4, 8.6 | |
| F16 |
3/10
|
Shock Losses, Compressible Flow Pitot-Tube
|
8.6, 8.7 | |
| F17 |
3/13
|
Oblique Shocks
|
9.1, 9.2 | |
| F18 |
3/15
|
Prandtl-Meyer Waves, Shock Expansion Theory
|
9.6, 9.7 | |
| F19 |
3/16
|
Compressible Channel Flow
|
10.1, 10.2 | |
| F20 |
3/20
|
Laval Nozzle Flows
|
10.3
|