Sylabus

Homework

Old Homework

Advanced Aerodynamics
Introduction to Analytical and
Computational Subsonic Aerodynamics

Sylabus

NACA 4-Digit Airfoil Solver (Java Applet)

Wing Vortex Program (Java Applet)

Lecture Slides :

Chapter 2, Part 1 : Review of Vectors and Calculus

Chapter 2, Part 2 : Flow Equations, Potential and Stream Functions

Chapter 3, Part 1 : Uniform Flow with Source

Chapter 3, Part 2 : Rankin Ovals, Doublets and Cylinders

Chapter 3, Part 3 : Distributed Source/Sinks

Chapter 3, Part 4 : Thin Airfoil Theory for Symmetric Shapes

Chapter 3, Part 5 : Source/Doublet Panel Methods

Chapter 4, Part 1 : Thin Airfoil Theory for Lifting Bodies

Chapter 4, Part 2 : Results from Thin Airfoil Theory

Chapter 5, Part 1 : Modeling of Wings, Hemholtz' Theorems

Chapter 5, Part 2 : Biot-Savart Law, Lifting Line Theory, Elliptical Loadings

Chapter 5, Part 3 : Non-Elliptical Loadings

Chapter 5, Part 4 : Vortex Lattice Method

Chapter 6, Part 1 : Compressible Potential Relations

Chapter 6, Part 2 : Small Perturbation Relations

Chapter 6, Part 3 : Prandlt-Glauert Similarity, Subsonic Wavy Wall

Chapter 6, Part 4 : Supersonic Wavy Wall

Chapter 6, Part 5 : Supersonic Conical Flow/Panel Method

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