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Early detection of thermoacoustic instabilities in a cryogenic rocket thrust chamber using combustion noise features and machine learning.

Chaos (Woodbury, N.Y.)

Waxenegger-Wilfing G, Sengupta U, Martin J, Armbruster W, Hardi J, Juniper M, Oschwald M.
PMID: 34241297
Chaos. 2021 Jun;31(6):063128. doi: 10.1063/5.0038817.

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 are used to train...

Academic Self-Concept: Modeling and Measuring for Science.

Research in Science Education

Hardy.
UIID-EM: 140
2014;44:549-579. doi: 10.1007/s11165-013-9393-7.

No abstract available.

Showing 925 to 926 of 926 entries