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An experimental investigation on the trailing edge cooling of turbine blades 被引量:5
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作者 Zifeng Yang Hui Hun 《Propulsion and Power Research》 SCIE 2012年第1期36-47,共12页
An experimental study was conducted to quantify the flow characteristics of the wall jets pertinent to trailing edge cooling of turbine blades.A high-resolution stereoscopic particle image velocimetry(PIV)system was u... An experimental study was conducted to quantify the flow characteristics of the wall jets pertinent to trailing edge cooling of turbine blades.A high-resolution stereoscopic particle image velocimetry(PIV)system was used to conduct detailed flow field measurements to quantitatively visualize the evolution of the unsteady vortices and turbulent flow structures in the cooling wall jet streams and to quantify the dynamic mixing process between the cooling jet stream and the mainstream flows.The detailed flow field measurements were correlated with the adiabatic cooling effectiveness maps measured by using pressure sensitive paint(PSP)technique to elucidate underlying physics in order to explore/optimize design paradigms for improved cooling effectiveness to protect the critical portions of turbine blades from harsh environments. 展开更多
关键词 Trailing edge cooling Wall slot jets Turbine blades Steroscopic particle image velocimetry(PIV)measurements Pressure sensitive paint(psp)technique
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