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This project delivered a custom aeroacoustic testing system for ARL-MLS at the University of Toronto to validate CFD and ML models. It features an open-jet wind tunnel, semi-anechoic enclosure, and high-resolution noise measurement. The prototype met design goals and enables reliable aeroacoustic research.
This project explores the minimum pulse density required for velvet noise to be subjectively perceived as Gaussian white noise when used in artificial reverberation.