Zero-crossing rate method as an efficient tool for combustion instability diagnosis

From National Research Council Canada

DOIResolve DOI: https://doi.org/10.1016/j.expthermflusci.2020.110340
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Affiliation
  1. National Research Council of Canada. Aerospace
FunderSearch for: Incheon National University
FormatText, Article
Subjectcombustion instability; zero-crossing rate; dynamic pressure; gas turbine combustor; stability margin
Abstract
Publication date
PublisherElsevier
In
LanguageEnglish
Peer reviewedYes
IdentifierS0894177720308384
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Record identifier9abaa387-15af-492a-a2d4-81f815d34f7e
Record created2023-06-16
Record modified2023-06-16
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