Advanced aerodynamics covering potential flow, wing theory, panel methods, and propeller theory.
Solve potential flow problems in the context of aerodynamics
Model and solve for the potential flow over airfoils using two-dimensional panel methods
Analyze the performance characteristics of two- and three-dimensional lifting surfaces, including interpreting data and computing lift and drag polars
Solve aerodynamics problems and interpret solutions using the appropriate non-dimensional parameters
Source: UW Guide
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MATH 321, (E M A 202, M E 240, or PHYSICS 311), and (CIV ENGR 310 or M E 363), or graduate/professional standing, or member of Engineering Guest Students
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Raw average: 4.29/5 from 7 quality ratings. The adjusted rating blends this with the UW review average (3.66/5), weighted as 20 additional ratings. Smaller samples stay closer to that average. Each captured review is counted once in the prior; this does not correct who chooses to leave a review.
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| Section | Mode | Enrolled / capacity | Waitlist |
|---|---|---|---|
| LEC 001 | Classroom Instruction | 0 / 60 | 0 |
| DIS 301 | Classroom Instruction | 0 / 28 | 0 |
| DIS 302 | Classroom Instruction | 0 / 28 | 0 |
Times are Central. Select a meeting for details; export includes recorded dates for the selected sections. Enrollment reflects scan time.
Potential flow theory; stream functions; vortex filaments and sheets. Two- and three-dimensional wing theory. Doublet and panels methods. Propeller theory. Was E M A 521 prior to Fall 2026.
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Aerodynamics
Recorded 2026-10-14[
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]Original comments behind the course and instructor summaries.
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Explore recorded gradesRecorded 2026-10-14
Recorded model configuration, reasoning, and tool conversations.
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