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contributor authorBruschewski, Martin
contributor authorScherhag, Christian
contributor authorSchiffer, Heinz
contributor authorGrundmann, Sven
date accessioned2017-05-09T01:34:11Z
date available2017-05-09T01:34:11Z
date issued2016
identifier issn0889-504X
identifier otherturbo_138_06_061005.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/162777
description abstractA study examining the internal cooling of turbine blades by swirling flow is presented. The sensitivity of swirling flow is investigated with regard to Reynolds number, swirl intensity, and the common geometric features of bladecooling ducts. The flow system consists of a straight and round channel that is attached to a swirl generator with tangential inlets. Different orifices and 180deg bends are employed as channel outlets. The experiments were carried out with magnetic resonance velocimetry (MRV) for which water was used as flow medium. As the main outcome, it was found that the investigated flows are highly sensitive to the conditions at the channel outlet. However, it was also discovered that for some outlet geometries the flow field remains the same. The associated flow features a favorable topology for heat transfer; the majority of mass is transported in the annular region close to the channel walls. Together with its high robustness, it is regarded as an applicable flow type for the internal cooling of turbine blades. A large eddy simulation (LES) was conducted to analyze the heat transfer characteristic of the associated flow for S0=3 and Re=20,000. The simulation showed an averaged Nusselt number increase of factor 4.7 compared to fully developed flow. However, a pressure loss increase of factor 43 must be considered as well.
publisherThe American Society of Mechanical Engineers (ASME)
titleInfluence of Channel Geometry and Flow Variables on Cyclone Cooling of Turbine Blades
typeJournal Paper
journal volume138
journal issue6
journal titleJournal of Turbomachinery
identifier doi10.1115/1.4032363
journal fristpage61005
journal lastpage61005
identifier eissn1528-8900
treeJournal of Turbomachinery:;2016:;volume( 138 ):;issue: 006
contenttypeFulltext


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