INTRODUCTION
Chapter II. Handout #1
Chapter II. Handout #2
Chapter II. Handout #3
Chapter II, Handout #4
Chapter III, Handout #1
Chapter III, Handout #2
Chapter III, Handout #3
Chapter III, Handout #4
Quiz II



Chapter IV. Handout I. Panel method
Panel Code in MATLAB
Panel Code input
Chapter IV. Handout II Starting Vortex
Chapter IV. Handout III Thin Airfoil Theory Terminology
Thin Airfoil Theory Derivation

Chapter V. Part I. Lifting Line Model
Chapter V. Part II. Biot-Savart Law
Chapter V. Part III. Lift and Drag Distribution
Chapter V. Part IV. Elliptically Loaded Wings
MATLAB Source Code for Analyzing arbitrary wings
Lifting Line Code from U. of Sydney, on the web

Home Work Set # 2

Home Work Set # 3

Home Work Set # 4

Home Work Set # 4 Hints

Home Work Set # 5