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

From National Research Council Canada

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  1. National Research Council of Canada. NRC Institute for Aerospace Research
FormatText, Article
ConferenceASME 1992 International Gas Turbine and Aeroengine Congress and Exposition, GT 1992, 1 June 1992 through 4 June 1992
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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Peer reviewedYes
NPARC number21275130
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Record identifier29ab8df4-45db-4ae8-922c-2947d3316302
Record created2015-05-11
Record modified2020-04-23
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