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AA210B - Fundamentals of Compressible Flow
Continuation of 210A with emphasis on more general flow geometry. Use of exact solutions to explore the hypersonic limit. Identification of similarity parameters. Solution methods for the linearized potential equation with applications to wings and bodies in steady flow; their relation to physical acoustics and wave motion in nonsteady flow. Nonlinear solutions for nonsteady constant area flow and introduction to Riemann invariants. Elements of the theory of characteristics; nozzle design; extension to nonisentropic flow. Real gas effects in compressible flow. Flows in various gas dynamic testing facilities. Prerequisite: 210A.
GERs: None
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2008-2009 Winter
| Sec | Type | Instructor | Room | Units | Days | Times | ||
|---|---|---|---|---|---|---|---|---|
| 01 | Lecture | Juan Alonso | TBA | 3 | Tue Thu | 1:15-2:30pm |
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