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contributor authorPichler, R.
contributor authorSandberg, R. D.
contributor authorMichelassi, V.
contributor authorBhaskaran, R.
date accessioned2017-05-09T01:34:26Z
date available2017-05-09T01:34:26Z
date issued2016
identifier issn0889-504X
identifier othergtp_138_11_112804.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/162832
description abstractIn the present paper, direct numerical simulation (DNS) data of a lowpressure turbine (LPT) are investigated in light of turbulence modeling. Many compressible turbulence models use Favreaveraged transport equations of the conservative variables and turbulent kinetic energy (TKE) along with other modeling equations. First, a general discussion on the turbulence modeling error propagation prescribed by transport equations is presented, leading to the terms that are considered to be of interest for turbulence model improvement. In order to give turbulence modelers means of validating their models, the terms appearing in the Favreaveraged momentum equations are presented along pitchwise profiles at three axial positions. These three positions have been chosen such that they represent regions with different flow characteristics. General trends indicate that terms related with thermodynamic fluctuations and Favre fluctuations are small and can be neglected for most of the flow field. The largest errors arise close to the trailing edge (TE) region where vortex shedding occurs. Finally, linear models and the scope for their improvement are discussed in terms of a priori testing. Using locally optimized turbulence viscosities, the improvement potential of widely used models is shown. On the other hand, this study also highlights the danger of pure local optimization.
publisherThe American Society of Mechanical Engineers (ASME)
titleInvestigation of the Accuracy of RANS Models to Predict the Flow Through a Low Pressure Turbine
typeJournal Paper
journal volume138
journal issue12
journal titleJournal of Turbomachinery
identifier doi10.1115/1.4033507
journal fristpage121009
journal lastpage121009
identifier eissn1528-8900
treeJournal of Turbomachinery:;2016:;volume( 138 ):;issue: 012
contenttypeFulltext


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