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RISCatalytic Combustion Systems for Microscale Gas Turbine Engines
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: As part of an ongoing effort to develop a microscale gas turbine engine for power generation and micropropulsion applications, this paper presents the design, modeling, and experimental assessment ...
Gas Turbine Engine Durability Impacts of High Fuel-Air Ratio Combustors—Part I: Potential for Secondary Combustion of Partially Reacted Fuel
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Demand for greater engine efficiency and thrust-to-weight ratio has driven the production of aircraft engines with higher core temperatures and pressures. Such engines operate at higher fuel-air ...
High Power Density Silicon Combustion Systems for Micro Gas Turbine Engines
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: As part of an effort to develop a microscale gas turbine engine for power generation and micropropulsion applications, this paper presents the design, fabrication, experimental testing, and ...
Endwall Blockage in Axial Compressors
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: This paper presents a new methodology for quantifying compressor endwall blockage and an approach, using this quantification, for defining the links between design parameters, flow conditions, and ...
Gas Turbine Engine Durability Impacts of High Fuel-Air Ratio Combustors—Part II: Near-Wall Reaction Effects on Film-Cooled Heat Transfer
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: As commercial and military aircraft engines approach higher total temperatures and increasing overall fuel-to-air ratios, the potential for significant chemical reactions on a film-cooled surface ...