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AA200A - Applied Aerodynamics
Fundamental equations of fluid dynamics and the physical assumptions on which they are based; overview of appropriate methods for solving these equations including nonlinear CFD, linear panel and vortex methods; estimation of pressure distributions and resultant airloads on 2-D airfoils, finite wings, slender bodies, and lifting systems; compressibility effects; boundary layer analysis and prediction of drag, separation, and displacement effects. Application to airfoil and wing design. Prerequisite: undergraduate aeronautics course. Recommended: 210A.
GERs: None
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2008-2009 Winter
| Sec | Kind | Books | ||
|---|---|---|---|---|
| 01 | Required Material(s) | Anderson: | Fund of Aerodynamics (4th ed) | $202.25 |
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