University of California, Berkeley 3 credits Mechanical Engineering
This course will cover the fundamentals of acoustics and the mathematical governing equations. Students will learn about the theory of aerodynamic noise sources and the numerical methods and metrics used to calculate the aerodynamic noise levels. Introduction to computational aeroacoustics will be covered and the process of setting up a simulation study to calculate acoustic signature due to aerodynamic pressure field will be described. The theory will be applied to aerospace use cases such as jet noise, rotor noise, urban air mobility (UAM) and drone noise. Students will get hands-on exposure of simulation setup to calculate aerodynamic noise.
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