Develop effective techniques for the aerodynamic analysis of aircraft, focusing on airfoil and finite wing theory. Equations of motion in differential and integral form and alternate forms of the equations with rotational and irrotational flow will be examined.
Biweekly assignments require MATLAB or a suitable programming language.
A conferred Bachelor’s degree with an undergraduate GPA of 3.5 or better.
Undergraduate courses in basic fluid mechanics and applied aerodynamics (Stanford Course: AA210A) or equivalent.
- Laminar-to-turbulent transition
- Two-dimensional laminar and turbulent boundary layers in airfoil analysis
- Far-field and Trefftz-plane analysis
- Compressibility effects and similarity rules
Note on Course Availability
The course schedule is displayed for planning purposes – courses can be modified, changed, or cancelled. Course availability will be considered finalized on the first day of open enrollment. For quarterly enrollment dates, please refer to our graduate education section
|Dates:||January 11 - March 19, 2021|
Pre-registration for this course will secure your enrollment request and ensure timely processing of your application for potential course approval. Please note: course enrollment will be confirmed after December 11, 2020; after completing your pre-registration, no further action is required on your part.
This course may not currently be available to learners in some states and territories.