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contributor authorZhao, Lei
contributor authorWang, Ting
date accessioned2017-05-09T01:13:42Z
date available2017-05-09T01:13:42Z
date issued2014
identifier issn0889-504X
identifier otherturb_136_07_071007.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/156630
description abstractA phase Doppler particle analyzer (PDPA) system is employed to measure the twophase mist flow behavior including flow velocity field, droplet size distribution, droplet dynamics, and turbulence characteristics. Based on the droplet measurements made through PDPA, a projected profile describing how the airmist coolant jet flow spreads and eventually blends into the hot main flow is proposed. This proposed profile is found to be well supported by the measurement results of the turbulent Reynolds stresses. The coolant film envelope is identified with shear layers characterized by higher magnitudes of turbulent Reynolds stresses. In addition, the separation between the mist droplet layer and the coolant air film is identified through the droplet measurements—large droplets penetrate through the air coolant film layer and travel further into the main flow. With the proposed airmist film profile, the heat transfer results on the wall presented in Part I are reexamined and more indepth physics is revealed. It is found that the location of the optimum cooling effectiveness coincides with the point where the airmist coolant stream starts to bend back towards the surface. Thus, the data suggests that the “bending backâ€‌ film pattern is critical in keeping the mist droplets close to the surface, which improves the cooling effectiveness for mist cooling.
publisherThe American Society of Mechanical Engineers (ASME)
titleAn Experimental Study of Mist/Air Film Cooling On a Flat Plate With Application to Gas Turbine Airfoils—Part II: Two Phase Flow Measurements and Droplet Dynamics
typeJournal Paper
journal volume136
journal issue7
journal titleJournal of Turbomachinery
identifier doi10.1115/1.4025738
journal fristpage71007
journal lastpage71007
identifier eissn1528-8900
treeJournal of Turbomachinery:;2014:;volume( 136 ):;issue: 007
contenttypeFulltext


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