Ice crystal accretion test rig development for a compressor transition duct

From National Research Council Canada

DOIResolve DOI: https://doi.org/10.2514/6.2010-7529
AuthorSearch for: 1; Search for: 1
Affiliation
  1. National Research Council of Canada. NRC Institute for Aerospace Research
FormatText, Article
ConferenceAIAA Atmospheric and Space Environments Conference 2010, 2 August 2010 through 5 August 2010, Toronto, ON
Subjectaircraft gas turbine engines; engine testing; gas turbine compressors; temperature data; test condition; test platforms; transition ducts; visual observations; aircraft; compressors; ducts; engines; gas turbines; ice
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LanguageEnglish
Peer reviewedYes
NPARC number21275132
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Record identifier63eddc70-15d4-408a-9436-716b1798ba7f
Record created2015-05-11
Record modified2020-04-17
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