Add to ORKGProtective coatings for heat resistant materials for aircraft gas turbine engines, and refractory metals for reentry vehicle
A wide range of programs are being conducted for improving the environmental resistance to oxidation...
Activities performed in order to provide an R&T data base for utility gas turbine systems burning co...
The Materials for Advanced Turbine Engine (MATE) Program managed by the NASA Lewis Research Center i...
The status of several coating programs is reviewed. These include efforts on protecting aircraft gas...
Recent activities of the Lewis Research Center are reviewed which are directed toward developing mat...
The NASA Lewis Research Center made technical assistance arrangements (contracts) with several comme...
A durable, two-layer, plasma-sprayed coating consisting of a ceramic layer over a metallic layer was...
Material categories as well as coatings and recent turbine cooling developments are reviewed. Curren...
A durable, two-layer, plasma-sprayed coating consisting of a ceramic layer over a metallic layer was...
The development of power and propulsion system technology is discussed. Specific emphasis is placed ...
The Materials Division at the Lewis Research Center has a long record of contributions to both mater...
Thin thermal barrier coatings for protecting aircraft turbine section airfoils are examined. The dis...
Methods currently used to deposit protective coatings in gas turbines are reviewed, and the structur...
Development of high temperature alloys, dispersion strengthened materials, composites, and coatings ...
Ceramic thermal barrier coating (TBC) system was tested by industrial and governmental organizations...
A wide range of programs are being conducted for improving the environmental resistance to oxidation...
Activities performed in order to provide an R&T data base for utility gas turbine systems burning co...
The Materials for Advanced Turbine Engine (MATE) Program managed by the NASA Lewis Research Center i...
The status of several coating programs is reviewed. These include efforts on protecting aircraft gas...
Recent activities of the Lewis Research Center are reviewed which are directed toward developing mat...
The NASA Lewis Research Center made technical assistance arrangements (contracts) with several comme...
A durable, two-layer, plasma-sprayed coating consisting of a ceramic layer over a metallic layer was...
Material categories as well as coatings and recent turbine cooling developments are reviewed. Curren...
A durable, two-layer, plasma-sprayed coating consisting of a ceramic layer over a metallic layer was...
The development of power and propulsion system technology is discussed. Specific emphasis is placed ...
The Materials Division at the Lewis Research Center has a long record of contributions to both mater...
Thin thermal barrier coatings for protecting aircraft turbine section airfoils are examined. The dis...
Methods currently used to deposit protective coatings in gas turbines are reviewed, and the structur...
Development of high temperature alloys, dispersion strengthened materials, composites, and coatings ...
Ceramic thermal barrier coating (TBC) system was tested by industrial and governmental organizations...
A wide range of programs are being conducted for improving the environmental resistance to oxidation...
Activities performed in order to provide an R&T data base for utility gas turbine systems burning co...
The Materials for Advanced Turbine Engine (MATE) Program managed by the NASA Lewis Research Center i...