The ability to characterize the interfacial delamination properties of thermal barrier coatings (TBCs) is of great technological importance for lifetime assessment of such coatings under service conditions. The purpose of this paper is to report on our novel experimental-plus-simulation-based approach to determine the relevant material parameters appearing in a traction-separation-type law which should be useful for modeling delamination failures in TBCs. We combine load–displacement measurements obtained from (i) a standard tension experiment; (ii) a novel shear experiment; and (iii) a novel asymmetric four-point bending mixed-mode experiment, with simulations of these experiments using a representative traction-separation law in a finite-...
Thermal barrier coatings are commonly used in high temperature parts of gas turbines, to protect the...
Thermal Barrier Coatings have been widely used in modern turbine engines to protect the nickel based...
This article describes a method of predicting the failure of a thermal barrier coating system due to...
A test technique has been developed to facilitate evaluation of the fracture characteristics of coat...
Mechanisms leading to degradation of the adherence of thermal barrier coatings (TBC) used in aircraf...
Mechanism-based lifetime assessment models of thermal barrier coating (TBC) systems for gas turbine ...
Mechanism-based lifetime assessment models of thermal barrier coating (TBC) systems rely on accurate...
Mechanism-based lifetime assessment models of thermal barrier coating (TBC) systems rely on accurate...
Instrumented indentation has been suggested as a method to determine interfacial fracture toughness ...
Reliable high-temperature propulsion materials are crucial to improved engine efficiency, reduced fu...
AbstractCatastrophic failure of thermal barrier coatings (TBCs), usually occurs due to large scale b...
Layered thermal barrier coating (TBC) systems used in jet engines consist of a nickel-based superall...
The present investigation deals with a plasma-sprayed thermal barrier coating (TBC) intended for hig...
Thermal barrier coating (TBC) is widely used to lower the temperature of turbine blades and prevent ...
Thermal barrier coatings are commonly used in high temperature parts of gas turbines, to protect the...
Thermal barrier coatings are commonly used in high temperature parts of gas turbines, to protect the...
Thermal Barrier Coatings have been widely used in modern turbine engines to protect the nickel based...
This article describes a method of predicting the failure of a thermal barrier coating system due to...
A test technique has been developed to facilitate evaluation of the fracture characteristics of coat...
Mechanisms leading to degradation of the adherence of thermal barrier coatings (TBC) used in aircraf...
Mechanism-based lifetime assessment models of thermal barrier coating (TBC) systems for gas turbine ...
Mechanism-based lifetime assessment models of thermal barrier coating (TBC) systems rely on accurate...
Mechanism-based lifetime assessment models of thermal barrier coating (TBC) systems rely on accurate...
Instrumented indentation has been suggested as a method to determine interfacial fracture toughness ...
Reliable high-temperature propulsion materials are crucial to improved engine efficiency, reduced fu...
AbstractCatastrophic failure of thermal barrier coatings (TBCs), usually occurs due to large scale b...
Layered thermal barrier coating (TBC) systems used in jet engines consist of a nickel-based superall...
The present investigation deals with a plasma-sprayed thermal barrier coating (TBC) intended for hig...
Thermal barrier coating (TBC) is widely used to lower the temperature of turbine blades and prevent ...
Thermal barrier coatings are commonly used in high temperature parts of gas turbines, to protect the...
Thermal barrier coatings are commonly used in high temperature parts of gas turbines, to protect the...
Thermal Barrier Coatings have been widely used in modern turbine engines to protect the nickel based...
This article describes a method of predicting the failure of a thermal barrier coating system due to...