This document describes work performed related to the determination of how elemental additions affect the interfacial fracture toughness of thermal barrier coatings at the bond coat/thermally grown oxide interface in gas turbines. These turbines are exposed to cyclical thermal loading, therefore a simulation was designed to model this interface in a temperature cycle between 200 K and 1000 K that included oxide growth between 2 μm and 27 μm. The fracture toughness of this interface was then determined to elucidate the function of elemental additions. It was shown that minimal concentrations of atomic species, such as hafnium and yttrium cause notable increases in the toughness of the bond coat/thermally grown oxide interface, while other sp...
The efficiency and reliability of modern jet engines strongly depend on the performance of thermal b...
Thermal Barrier Coating (TBC) systems are protective layers applied to critical structural component...
The efficiency and reliability of modern jet engines strongly depend on the performance of thermal b...
A method is presented that allows determination of the work of adhesion between oxides and metals us...
A method is presented that allows determination of the work of adhesion between oxides and metals us...
A method is presented that allows determination of the work of adhesion between oxides and metals us...
Ceramic thermal barrier coatings represent an attractive method of increasing the high temperature l...
A method is presented that allows determination of the work of adhesion between oxides and metals us...
A method is presented that allows determination of the work of adhesion between oxides and metals us...
Gas turbine materials exposed to extreme high temperature require protective coatings. To design rel...
Gas turbine materials exposed to extreme high temperature require protective coatings. To design rel...
A method is presented that allows determination of the work of adhesion between oxides and metals us...
Gas turbine materials exposed to extreme high temperature require protective coatings. To design rel...
High pressure turbine blades in gas turbine engines rely on thermal barrier coating (TBC) systems fo...
The efficiency and reliability of modern jet engines strongly depend on the performance of thermal b...
The efficiency and reliability of modern jet engines strongly depend on the performance of thermal b...
Thermal Barrier Coating (TBC) systems are protective layers applied to critical structural component...
The efficiency and reliability of modern jet engines strongly depend on the performance of thermal b...
A method is presented that allows determination of the work of adhesion between oxides and metals us...
A method is presented that allows determination of the work of adhesion between oxides and metals us...
A method is presented that allows determination of the work of adhesion between oxides and metals us...
Ceramic thermal barrier coatings represent an attractive method of increasing the high temperature l...
A method is presented that allows determination of the work of adhesion between oxides and metals us...
A method is presented that allows determination of the work of adhesion between oxides and metals us...
Gas turbine materials exposed to extreme high temperature require protective coatings. To design rel...
Gas turbine materials exposed to extreme high temperature require protective coatings. To design rel...
A method is presented that allows determination of the work of adhesion between oxides and metals us...
Gas turbine materials exposed to extreme high temperature require protective coatings. To design rel...
High pressure turbine blades in gas turbine engines rely on thermal barrier coating (TBC) systems fo...
The efficiency and reliability of modern jet engines strongly depend on the performance of thermal b...
The efficiency and reliability of modern jet engines strongly depend on the performance of thermal b...
Thermal Barrier Coating (TBC) systems are protective layers applied to critical structural component...
The efficiency and reliability of modern jet engines strongly depend on the performance of thermal b...