Influence of a thermal barrier coating on the performance of a turboprop engine

From National Research Council Canada

DOIResolve DOI: http://doi.org/10.1115/92-GT-038
AuthorSearch for: 1 ; Search for:
Name affiliation
  1. National Research Council Canada. NRC Institute for Aerospace Research
TypeArticle
Proceedings titleASME 1992 International Gas Turbine and Aeroengine Congress and Exposition, GT 1992
ConferenceASME 1992 International Gas Turbine and Aeroengine Congress and Exposition, GT 1992, 1 June 1992 through 4 June 1992
ISBN9780791878941
Volume2
SubjectAircraft engines; Ceramic coatings; Ceramic materials; Coatings; Engines; Marine engines; Nozzles; Surface roughness; Thermal barrier coatings; Thickness measurement; Turbine components; Uncertainty analysis; Canadian department of national defence; Coating application; Experimental installations; Measurement uncertainty analysis; National Research Council of Canada; Performance variations; Project objectives; Turbine inlet temperature; Gas turbines
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LanguageEnglish
Peer reviewedYes
NPARC number21275130
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Record created2015-05-11
Record modified2016-05-09
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