Instructor

Juan J. Alonso
Durand Bldg. Room 365
Department of Aeronautics & Astronautics
Stanford University
Stanford, CA 94305

e-mail: jjalonso@stanford.edu
Tel: (650) 723-9954
Fax: (650) 725-3377

Office Hours

TBD

Course Syllabus

A tentative syllabus for the course can be found below.

Date Lecture No. Topic Lecture Notes
1/4 1 Introduction. Airfoil Characteristics. Airfoil Design Problems. Lecture 1 notes
1/6 2 Lifting Airfoils in Incompressible Irrotational Flow Lecture 2 notes
1/11 3 Lifting Airfoils and the Hess-Smith Panel Method Lecture 3 notes
1/13 4 The Hess-Smith Panel Method and Airfoil Characteristics Lecture 4 notes
1/18 5 Supersonic Thin Airfoil Theory Lecture 5 notes
1/20 6 The Boundary Layer Approximation Lecture 6 notes
1/25 7 Analytic Solutions and the VonKarman Integral Momentum Equations Lecture 7 notes
1/27 8 Integral Solution of Laminar Flows - Thwaites' Method Lecture 8 notes
2/1 9 Turbulent Boundary Layers and Their Integral Solution Lecture 9 notes
2/3 10 Transition Prediction and Modelling. Lecture 10 notes
2/8 11 MIDTERM EXAM
2/10 12 Airfoil Design Methods and Examples Lecture 12 notes
2/15 13 The Finite Wing. Introduction to Induced Drag Lecture 11 notes
2/17 14 Finite-Wing Details. Non-Elliptic Spanload Distributions Lecture 14 notes
2/22 15 Induced Drag Computation in the Trefftz Plane Lecture 15 notes
2/24 16 Induced Drag Computation in the Trefftz Plane (2) Lecture 16 notes
3/1 17 Induced Drag Minimization Lecture 17 notes
3/3 18 Non-planar and Multiple Lifting Surface Configurations. Winglets Lecture 18 notes
3/8 19 Wing Design - Lift Distributions and Performance Lecture 19 notes
3/10 20 Aerodynamic Shape Optimization Using the Euler and Navier-Stokes Equations Lecture 20 notes

Mon Jan 3 15:15:51 PST 2005
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