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RISGas Turbine Blade Heat Transfer and Internal Swirl Cooling Flow Experimental Study Using Liquid Crystals and Three-Dimensional Stereo-Particle Imaging Velocimetry
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: The challenging engineering intricacies related to improving efficiency of a gas turbine engine come with the need to maximize the internal cooling of the turbine blade to withstand the high turbine inlet temperature. ...
Application of a Ranque–Hilsch Vortex Flow in an Internal Cooling of a Gas Turbine Engine Blade
Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: The efficiency of a gas turbine engine is directly impacted by the turbine inlet temperature and the corresponding pressure ratio. A major strategy, aside from the use of costly high-temperature blade materials, is increasing ...