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Study of Turbulent Flow of Film Cooling Holes with Lateral Expanded Exits 被引量:3
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作者 施红辉 佐佐俊祐 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2002年第4期200-207,共8页
Hot wire measurements and flow visualization are presented for studying the turbulent flow field over a flat gas turbine film cooling blade with lateral expanded holes. Three mass flux ratios of jet to free stream, M ... Hot wire measurements and flow visualization are presented for studying the turbulent flow field over a flat gas turbine film cooling blade with lateral expanded holes. Three mass flux ratios of jet to free stream, M = 0.5, 0.89, 1.5, are tested. The streamwise velocity, the turbulent intensities and the Reynolds shear stress are measured. The effect of the lateral expanded holes on the improvement of the turbulent flow field for film cooling of gas turbines can be analyzed from the measured spatial di... 展开更多
关键词 turbulent flow film cooling lateral expanded hole hot wire anemometry flow visualization
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