Early Detection of Thermoacoustic Instabilities in a Cryogenic Rocket Thrust Chamber using Combustion Noise Features and Machine Learning
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DOI: 10.1063/5.0038817
Abstract: We present a data-driven method for the early detection of thermoacoustic instabilities. Recurrence quantification analysis is used to calculate characteristic combustion features from short-length time series of dynamic pressure sensor data. Features like recurrence rate… read more here.
Keywords: detection thermoacoustic; early detection; combustion; thrust chamber ... See more keywords