The high-cycle fatigue of composite stator vanes provided an accelerated life-state prior to insertion in a test stand engine. The accelerated testing was performed in the Structural Dynamics Laboratory at the NASA Glenn Research Center under the guidance of Structural Mechanics and Dynamics Branch personnel. Previous research on fixturing and test procedures developed at Glenn determined that engine vibratory conditions could be simulated for polymer matrix composite vanes by using the excitation of a combined slip table and electrodynamic shaker in Glenn's Structural Dynamics Laboratory. Bench-top testing gave researchers the confidence to test the coated vanes in a full-scale engine test
The Naval Weapons Center at China Lake, California is currently evaluating a counter rotating propfa...
The technology of plasma sprayed thermal barrier coatings applied to turbine vane platforms in moder...
The use of ceramic matrix composites (CMCs) as vanes for the next generation of turbine engines is u...
Both the NASA Glenn Research Center and the Allison Advanced Development Company (AADC) have worked ...
A program was conducted by NASA with the JT9D engine manufacturer to develop a lightweight, cost eff...
An integrated team of NASA personnel, Government contractors, industry partners, and university staf...
There is a need for lightweight, durable materials and structures to reduce the weight of propulsion...
FAA fan blade-out certification testing on turbofan engines occurs very late in an engine's developm...
A series of programs were conducted to investigate and develop the application of composite material...
As part of a NASA program to reduce fuel consumption of current commercial aircraft engines, methods...
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1998.In...
The Lewis Research Center is conducting a series of programs intended to investigate and develop the...
A series of mechanical load tests was completed on several novel design concepts for extremely light...
The Federal Aviation Administration is working with the European Aviation Safety Agency to determine...
Plasma-Sprayed ceramic coatings are an appealing alternative to shrouded vane interstage labyrinth s...
The Naval Weapons Center at China Lake, California is currently evaluating a counter rotating propfa...
The technology of plasma sprayed thermal barrier coatings applied to turbine vane platforms in moder...
The use of ceramic matrix composites (CMCs) as vanes for the next generation of turbine engines is u...
Both the NASA Glenn Research Center and the Allison Advanced Development Company (AADC) have worked ...
A program was conducted by NASA with the JT9D engine manufacturer to develop a lightweight, cost eff...
An integrated team of NASA personnel, Government contractors, industry partners, and university staf...
There is a need for lightweight, durable materials and structures to reduce the weight of propulsion...
FAA fan blade-out certification testing on turbofan engines occurs very late in an engine's developm...
A series of programs were conducted to investigate and develop the application of composite material...
As part of a NASA program to reduce fuel consumption of current commercial aircraft engines, methods...
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1998.In...
The Lewis Research Center is conducting a series of programs intended to investigate and develop the...
A series of mechanical load tests was completed on several novel design concepts for extremely light...
The Federal Aviation Administration is working with the European Aviation Safety Agency to determine...
Plasma-Sprayed ceramic coatings are an appealing alternative to shrouded vane interstage labyrinth s...
The Naval Weapons Center at China Lake, California is currently evaluating a counter rotating propfa...
The technology of plasma sprayed thermal barrier coatings applied to turbine vane platforms in moder...
The use of ceramic matrix composites (CMCs) as vanes for the next generation of turbine engines is u...