AE 264 - Gas Dynamics

3 unit(s)
Advanced topics in compressible flow theory with emphasis on the design of high subsonic, supersonic and hypersonic vehicles. In addition to classical compressible flow theory and problem solving, the course may include supersonic wind tunnel experiments and computer simulations.

Prerequisite(s): BS Aerospace Engineering or BS Mechanical Engineering or instructor consent.
Grading: Letter Graded

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