16.120 Compressible Internal Flow and Aeroacoustics
Internal compressible flow and fundamentals of acoustics and aerodynamic sound with applications in turbomachinery and propulsion systems. Quasi-one-dimensional compressible flow (channel flow) and extensions, including effects of shock waves, friction, energy and mass addition, swirl, and flow non-uniformity. Unsteady compressible flow, theory of sound, sources of sound and wave propagation, Lighthill's acoustic analogy, and characterization and estimation of noise sources encountered in turbomachinery and aircraft applications.
This class has 2.25 as a prerequisite.
This class counts for a total of 12 credits. This is a graduate-level class.
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