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AA210A - Fundamentals of Compressible Flow
Topics: development of the three-dimensional, non-steady, field equations for describing the motion of a viscous, compressible fluid; differential and integral forms of the equations; constitutive equations for a compressible fluid; the entropy equation; compressible boundary layers; area-averaged equations for one-dimensional steady flow; shock waves; channel flow with heat addition and friction; flow in nozzles and inlets; oblique shock waves; Prandtl-Meyer expansion; unsteady one-dimensional flow; the shock tube; small disturbance theory; acoustics in one-dimension; steady flow in two-dimensions; potential flow; linearized potential flow; lift and drag of thin airfoils. Prerequisites: undergraduate background in fluid mechanics and thermodynamics.
GERs: None
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2007-2008 Autumn
| Sec | Kind | Books | ||
|---|---|---|---|---|
| 01 | Required Material(s) | Cantwell: | AA 210A Course Reader | |
| 01 | Recommended Material(s) | Van Dyke: | Album of Fluid Motion | |
2008-2009 Autumn
| Sec | Kind | Books | ||
|---|---|---|---|---|
| 01 | Required Material(s) | Cantwell: | AA 210A COURSE READER | |
| 01 | Recommended Material(s) | Van Dyke: | Album of Fluid Motion | |
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