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contributor authorShao, Hongyi
contributor authorQenawy, Mohamed
contributor authorZhang, Tianlun
contributor authorPeng, Di
contributor authorLiu, Yingzheng
contributor authorZhou, Wenwu
date accessioned2022-02-05T22:06:49Z
date available2022-02-05T22:06:49Z
date copyright12/28/2020 12:00:00 AM
date issued2020
identifier issn0889-504X
identifier otherturbo_143_1_011002.pdf
identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4276938
description abstractAn experimental study was conducted to investigate the influence of mainstream oscillations on spatio-temporal variation of leading-edge film cooling effectiveness. The investigation utilized fast-response pressure-sensitive paint (Fast-PSP) technique at high frame rate. During the experiment, coolant (i.e., CO2, DR = 1.53) was discharged into three rows of cylindrical holes. Various blowing ratios (i.e., M = 0.50, 0.75, 1.00, and 1.50) were tested under the steady (i.e., f = 0 Hz) and oscillating (i.e., f = 7 Hz and 25 Hz) conditions. The measured instantaneous effectiveness was analyzed in terms of time-averaged and phase-averaged results. The results revealed that the mainstream oscillation, consisting of simultaneous pressure and velocity oscillation, significantly influences the behavior of the film cooling effectiveness. The time-averaged effectiveness significantly decreased at high oscillating frequency (i.e., 13.0–19.8% reduction at M = 0.50, f = 25 Hz compared with f = 0 Hz), especially at low blowing ratios (i.e., M = 0.50 and 0.75). The phase-averaged results captured significant decay in the film distributions associated with backflow caused by negative pressure gradients in coolant holes at certain phases. However, the mainstream oscillation effect was relatively insignificant at high blowing ratios (i.e., M = 1.00 and 1.50), which revealed the robustness of coolant coverage at low coolant Strouhal number (i.e., high blowing ratio) under the same oscillating frequency. Furthermore, the unsteady coolant intermittency showed highly unstable film coverage at high coolant Strouhal number. The coolant decay associated with backflow at high coolant Strouhal number should be considered by the gas-turbine designers in order to improve the lifecycle of turbine blades.
publisherThe American Society of Mechanical Engineers (ASME)
titleExperimental Study of Oscillating Freestream Effect on the Spatiotemporal Distributions of Leading-Edge Film Cooling
typeJournal Paper
journal volume143
journal issue1
journal titleJournal of Turbomachinery
identifier doi10.1115/1.4048794
journal fristpage011002-1
journal lastpage011002-15
page15
treeJournal of Turbomachinery:;2020:;volume( 143 ):;issue: 001
contenttypeFulltext


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