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RISAnalytical Study of Articulating Turbine Rotor Blade Concept for Improved Off-Design Performance of Gas Turbine Engines
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Gas turbine engines are generally optimized to operate at nearly a fixed speed with fixed blade geometries for the design operating condition. When the operating condition of the engine changes, the flow incidence angles ...
Molten Particulate Impact on Tailored Thermal Barrier Coatings for Gas Turbine Engine
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Commercial/military fixed-wing aircraft and rotorcraft engines often have to operate in significantly degraded environments consisting of sand, dust, ash, and other particulates. Marine gas turbine engines are subjected ...