Most of the efforts in the HOST Surface Protection Subproject were focused on thermal barrier coating (TBC) life prediction. Also, a small effort, consisting primarily of wrapping up and reporting the work of previous years, remained on the airfoil deposition modeling. The work performed under the airfoil deposition modeling program element was concerned with modeling the deposition of corrodants onto turbine airfoils. Accomplishments included verification of the chemically frozen boundary (CFBL) theory. Encouraging results were also achieved with the recently developed local thermochemical equilibrium (LTCE) theory. The surface protection subprogram was devoted to thermal-barrier-coating life modeling. This modeling is an essential step in...
A 0.025 cm (0.010 in) thick thermal barrier coating (TBC) applied to turbine airfoils in a research ...
The objectives of this program are to determine the predominant modes of degradation of a plasma spr...
This report describes the work performed on a thermal barrier coating support technology task of the...
Thermal barrier coatings (TBCs) for turbine airfoils in high-performance engines represent an advanc...
The program focuses on predicting the lives of two types of strain-tolerant and oxidation-resistant ...
A methodology was established to predict thermal barrier coating life in an environment simulative o...
A methodology is established to predict thermal barrier coating life in a environment similar to tha...
The objective is to develop an integrated life prediction model accounting for all potential life-li...
Life predictions are made for two types of strain-tolerant and oxidation-resistant Thermal Barrier C...
Thin thermal barrier coatings for protecting aircraft turbine section airfoils are examined. The dis...
Thermal Barrier Coatings (TBC), provide thermal insulation and oxidation resistance in an environmen...
Thermal barrier coating life models developed under the NASA Lewis Research Center's Hot Section Tec...
A lifing model has been developed based on lab testing to describe the time-temperature-dependence o...
This report describes work performed to determine the predominat modes of degradation of a plasma sp...
This is the second annual report of the first 3-year phase of a 2-phase, 5-year program. The objecti...
A 0.025 cm (0.010 in) thick thermal barrier coating (TBC) applied to turbine airfoils in a research ...
The objectives of this program are to determine the predominant modes of degradation of a plasma spr...
This report describes the work performed on a thermal barrier coating support technology task of the...
Thermal barrier coatings (TBCs) for turbine airfoils in high-performance engines represent an advanc...
The program focuses on predicting the lives of two types of strain-tolerant and oxidation-resistant ...
A methodology was established to predict thermal barrier coating life in an environment simulative o...
A methodology is established to predict thermal barrier coating life in a environment similar to tha...
The objective is to develop an integrated life prediction model accounting for all potential life-li...
Life predictions are made for two types of strain-tolerant and oxidation-resistant Thermal Barrier C...
Thin thermal barrier coatings for protecting aircraft turbine section airfoils are examined. The dis...
Thermal Barrier Coatings (TBC), provide thermal insulation and oxidation resistance in an environmen...
Thermal barrier coating life models developed under the NASA Lewis Research Center's Hot Section Tec...
A lifing model has been developed based on lab testing to describe the time-temperature-dependence o...
This report describes work performed to determine the predominat modes of degradation of a plasma sp...
This is the second annual report of the first 3-year phase of a 2-phase, 5-year program. The objecti...
A 0.025 cm (0.010 in) thick thermal barrier coating (TBC) applied to turbine airfoils in a research ...
The objectives of this program are to determine the predominant modes of degradation of a plasma spr...
This report describes the work performed on a thermal barrier coating support technology task of the...