Journal of Konbin
 2010
DOI: 10.2478/v10040-008-0158-8
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Analysis of Feasibility to Assess Microstructure of Gas Turbine Blades by Means of the Thermographic Method

Artur Kułaszka1,
Józef Błachnio2,
Łukasz Kornas3

Abstract: Operation of avionic turbine engines is always associated with possibility of various defects that may happen to turbine components, in particular to its blades. The most frequent reason for defects is overheating of the blade

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