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contributor authorSchreivogel, Peter
contributor authorPfitzner, Michael
date accessioned2017-05-09T01:34:03Z
date available2017-05-09T01:34:03Z
date issued2016
identifier issn0889-504X
identifier otherturbo_138_03_031003.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/162746
description abstractA new approach for steadystate heat transfer measurements is proposed. Temperature distributions are measured at the surface and a defined depth inside the wall to provide boundary conditions for a threedimensional heat flux calculation. The practical application of the technique is demonstrated by employing a superposition method to measure heat transfer and film cooling effectiveness downstream of two different 0.75D deep narrow trench geometries and cylindrical holes. Compared to the cylindrical holes, both trench geometries lead to an augmentation of the heat transfer coefficient supposedly caused by the highly turbulent attached cooling film emanating from the trenches. Areas of high heat transfer are visible, where recirculation bubbles or large amounts of coolant are expected. Increasing the density ratio from 1.33 to 1.60 led to a slight reduction of the heat transfer coefficient and an increased cooling effectiveness. Both trenches provide a net heat flux reduction (NHFR) superior to that of cylindrical holes, especially at the highest momentum flux ratios.
publisherThe American Society of Mechanical Engineers (ASME)
titleHeat Transfer Measurements Downstream of Trenched Film Cooling Holes Using a Novel Optical Two Layer Measurement Technique
typeJournal Paper
journal volume138
journal issue3
journal titleJournal of Turbomachinery
identifier doi10.1115/1.4031919
journal fristpage31003
journal lastpage31003
identifier eissn1528-8900
treeJournal of Turbomachinery:;2016:;volume( 138 ):;issue: 003
contenttypeFulltext


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