Topic

2/11

New F1, actually F18 from last semester, covering vortex sheets

2/12

Airfoil Vortex Sheet Models, Thin Airfoil Analysis Problem

2/17

Thin Airfoil Analysis Problem, Continued

Lecture F3
Thin Airfoil Theory glossary

2/24

Thin Airfoil Theory Application: Analysis Example

2/25

Introduction to 3D Wings, 2D and 3D Coefficients

2/27

3D Vortex Filaments, Lifting Line Theory

3/2

Elliptical Lift Distribution

3/5

Wing Geometry, Wing Design Problem

3/9

General Wings

3/10

Aircraft Performance Analysis

Lecture F10

Drag Estimation Table

4/8

Intorduction to Compressible Flows, Thermodynamic Concepts

7.1-7.2

4/10

Energy Conservation

4/17

Stagnation Quantities, Introduction to Shock Waves

4/22

Normal Shock Waves, Speed of Sound

4/24

Mach Number Relations, Normal Shock Properties

4/27

Shock Losses, Compressible Flow Pitot-Tube

4/28

Oblique Shocks

5/1

Prandtl-Meyer Waves, Shock Expansion Theory

5/4

Compressible Channel Flow

5/8

Laval Nozzle Flows

Lecture F20

Laval Notes

10.3