Abstract The results of experimental studies of the thermal conductivity coefficient of thermal barrier coatings (TBC) are presented. A technique for its determination is proposed and tested. The data of design evaluation of the TBC thickness distribution along the outline of a cooled turbine blade are given.
Thermal conductivity of thermal barrier coatings
Russian Aeronautics (Iz VUZ) ; 52 , 3 ; 340-346
2009-09-01
7 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
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