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Effects of Coolant Density, Specific Heat Capacity, and Biot Number on Turbine Vane Cooling Effectiveness
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: This paper describes the effects of coolant-to-mainstream density ratio and specific heat capacity flux ratio (the product of blowing ratio and specific heat capacity ratio) on the overall cooling effectiveness of high ...
Scaling of Turbine Metal Temperatures in Cooled Compressible Flows—Experimental Demonstration of a New Theory
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Experimental measurements of overall cooling effectiveness conducted on a high-pressure turbine vane in a warm rig flow are scaled to engine conditions in this paper. A new theory for the scaling of turbine metal temperatures ...
Design and Testing of a Multi-Stage Intermediate Pressure Turbine for Future Geared Turbofans
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: The multi-stage intermediate pressure turbine (IPT) is a key enabler of the thermodynamic cycle in geared turbofan engine architectures, where fan and turbine rotational speeds become decoupled by using a power gearbox ...
A New Transient High Heat Flux Convection Calibration Facility for Heat Transfer Gauges in High Enthalpy Flows
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: This paper presents a novel transient method for calibrating heat transfer gauges for convective wall heat flux measurements in high enthalpy flows. The new method relies on the transient heating of sensor substrates under ...
Full Thermal Experimental Assessment of a Dendritic Turbine Vane Cooling Scheme
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: A full thermal experimental assessment of a novel dendritic cooling scheme for highpressure turbine vanes has been conducted and is presented in this paper, including a comparison to the current stateoftheart cooling ...
A New Experimental Facility to Investigate Combustor–Turbine Interactions in Gas Turbines With Multiple Can Combustors
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: This paper describes a new modular experimental facility that was purposebuilt to investigate flow interactions between the combustor and first stage nozzle guide vanes (NGVs) of heavy duty power generation gas turbines ...
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