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contributor authorAn, Bai-Tao
contributor authorLiu, Jian-Jun
contributor authorZhou, Si-Jing
date accessioned2019-02-28T11:09:23Z
date available2019-02-28T11:09:23Z
date copyright6/14/2018 12:00:00 AM
date issued2018
identifier issn0889-504X
identifier otherturbo_140_07_071003.pdf
identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4253269
description abstractFilm-cooling effectiveness of rectangular diffusion holes under an inclination angle α = 45 deg, an orientation angle β = 45 deg, and a length-to-diameter ratio of L/D = 8.5 were, respectively, examined in a flat-plate experimental facility using the pressure sensitive paint (PSP) technique. Experiments were performed at a density ratio of DR = 1.38 and a mainstream turbulence intensity of Tu = 3.5%. The semicircle sidewall rectangular diffusion hole varied at three cross-sectional aspect ratios, i.e., AS = 3.4, 4.9, and 6.6. The tested results were compared with the baseline design with an inclination angle α = 30 deg, an orientation angle β = 0 deg, and a length-to-diameter ratio L/D = 6. A three-dimensional (3D) numerical simulation method was employed to analyze the flow field. The experimental results showed that the increased inclination angle converted the bi- or tri-peak effectiveness pattern of the baseline design to a single-peak pattern, weakened the lateral diffusion of coolant, and consequently decreased cooling effectiveness obviously. The decreased magnitude amplified with the increase of cross-sectional aspect ratio and blowing ratio. The adding of orientation angle seriously weakened the cooling effectiveness of the baseline design, and the blowing ratio and cross-sectional aspect ratio had almost no effect on overall cooling effectiveness. The elongated hole length provided a uniform distribution of lateral cooling effectiveness, which produced differential effects on the bi- or tri-peak pattern. The elongated hole length decreased the cooling effectiveness on the near hole region, but had less effects on overall cooling effectiveness, except the high blowing ratio.
publisherThe American Society of Mechanical Engineers (ASME)
titleEffects of Inclination Angle, Orientation Angle, and Hole Length on Film Cooling Effectiveness of Rectangular Diffusion Holes
typeJournal Paper
journal volume140
journal issue7
journal titleJournal of Turbomachinery
identifier doi10.1115/1.4040101
journal fristpage71003
journal lastpage071003-13
treeJournal of Turbomachinery:;2018:;volume 140:;issue 007
contenttypeFulltext


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