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

DOIResolve DOI: http://doi.org/10.1115/92-GT-038
AuthorSearch for: ; Search for:
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
Abstract
Publication date
LanguageEnglish
AffiliationNRC Institute for Aerospace Research; National Research Council Canada
Peer reviewedYes
NPARC number21275130
Export citationExport as RIS
Report a correctionReport a correction
Record identifier29ab8df4-45db-4ae8-922c-2947d3316302
Record created2015-05-11
Record modified2016-05-09
Bookmark and share
  • Share this page with Facebook (Opens in a new window)
  • Share this page with Twitter (Opens in a new window)
  • Share this page with Google+ (Opens in a new window)
Date modified: