High temperature mechanical properties of thermal barrier coated superalloy applied to combustor liner of aero engines

High Temperature Materials and Processes

Volumn 25, Issue 3, 2006, Pages 109-119

  Ray, A K ^a   Roy, N ^a   Dash, B ^a   Das, D K ^b   Ranganath, V R ^c   Goswami, B ^d   Singh, M P ^d   Tiwari, Y N ^a   Roy, P K ^a   Das, H K ^a   Sanyal, D ^e   Dwarakadasa, E S ^f  

^a NATIONAL METALLURGICAL LABORATORY   (India)

^b DEFENCE METALLURGICAL RESEARCH LABORATORY   (India)

^c SURFACE ENGINEERING DIVISION   (India)

^d RVS College of Engineering and Technology   (India)

^e CSIR CENTRAL GLASS AND CERAMIC RESEARCH INSTITUTE   (India)

^f INDIAN INSTITUTE OF SCIENCE   (India)

Author keywords

Creep; Fatigue; Finite element; Fractography; Intergranular; Spallation; Substrate; Tensile; Thermal barrier coating; Trans granular

Indexed keywords

ACOUSTIC EMISSION TESTING; COMBUSTORS; DELAMINATION; FINITE ELEMENT METHOD; FRACTOGRAPHY; HIGH TEMPERATURE EFFECTS; STRESSES; THERMAL BARRIER COATINGS;

DBTT (DUCTILE TO BRITTLE TRANSITION TEMPERATURE); INTERGRANULAR; SPALLATION;

MECHANICAL PROPERTIES;

EID: 33750010452     PISSN: 03346455     EISSN: None     Source Type: Journal    
DOI: 10.1515/HTMP.2006.25.3.109     Document Type: Article

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