Add to ORKGThe status of several coating programs is reviewed. These include efforts on protecting aircraft gas turbine engine materials from oxidation/corrosion and on protecting refractory metal reentry heat shields from oxidation
Methods currently used to deposit protective coatings in gas turbines are reviewed, and the structur...
The materials problem in the space shuttle main engine (SSME) is reviewed. Potential coatings and th...
A two-layer thermal barrier coating system with a bond coating of nickel-chromium-aluminum-yttrium a...
Protective coatings for heat resistant materials for aircraft gas turbine engines, and refractory me...
A durable, two-layer, plasma-sprayed coating consisting of a ceramic layer over a metallic layer was...
A durable, two-layer, plasma-sprayed coating consisting of a ceramic layer over a metallic layer was...
The NASA Lewis Research Center made technical assistance arrangements (contracts) with several comme...
A wide range of programs are being conducted for improving the environmental resistance to oxidation...
Thin thermal barrier coatings for protecting aircraft turbine section airfoils are examined. The dis...
Material categories as well as coatings and recent turbine cooling developments are reviewed. Curren...
Recent activities of the Lewis Research Center are reviewed which are directed toward developing mat...
High Temperature issues in aircraft engines Hot section: Ni and Co based Superalloys Oxidation and C...
Ceramic thermal barrier coating (TBC) system was tested by industrial and governmental organizations...
NASA has played a central role in the development of thermal barrier coatings (TBCs) for gas turbine...
Activities performed in order to provide an R&T data base for utility gas turbine systems burning co...
Methods currently used to deposit protective coatings in gas turbines are reviewed, and the structur...
The materials problem in the space shuttle main engine (SSME) is reviewed. Potential coatings and th...
A two-layer thermal barrier coating system with a bond coating of nickel-chromium-aluminum-yttrium a...
Protective coatings for heat resistant materials for aircraft gas turbine engines, and refractory me...
A durable, two-layer, plasma-sprayed coating consisting of a ceramic layer over a metallic layer was...
A durable, two-layer, plasma-sprayed coating consisting of a ceramic layer over a metallic layer was...
The NASA Lewis Research Center made technical assistance arrangements (contracts) with several comme...
A wide range of programs are being conducted for improving the environmental resistance to oxidation...
Thin thermal barrier coatings for protecting aircraft turbine section airfoils are examined. The dis...
Material categories as well as coatings and recent turbine cooling developments are reviewed. Curren...
Recent activities of the Lewis Research Center are reviewed which are directed toward developing mat...
High Temperature issues in aircraft engines Hot section: Ni and Co based Superalloys Oxidation and C...
Ceramic thermal barrier coating (TBC) system was tested by industrial and governmental organizations...
NASA has played a central role in the development of thermal barrier coatings (TBCs) for gas turbine...
Activities performed in order to provide an R&T data base for utility gas turbine systems burning co...
Methods currently used to deposit protective coatings in gas turbines are reviewed, and the structur...
The materials problem in the space shuttle main engine (SSME) is reviewed. Potential coatings and th...
A two-layer thermal barrier coating system with a bond coating of nickel-chromium-aluminum-yttrium a...