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contributor authorPrzytarski, Pawel J.
contributor authorWheeler, Andrew P. S.
date accessioned2022-02-05T22:07:40Z
date available2022-02-05T22:07:40Z
date copyright3/1/2021 12:00:00 AM
date issued2021
identifier issn0889-504X
identifier otherturbo_143_3_031008.pdf
identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4276966
description abstractFurther improvements in aero-engine efficiencies require accurate prediction of flow physics and incurred loss. Currently, the computational requirements for capturing these are not known leading to inconsistent loss predictions even for scale-resolving simulations depending on the chosen convergence criteria. This work investigates two aspects of loss generation using high-fidelity simulation. In the first case study, we look at the effect of resolution on capturing entropy generation rate by simulating a Taylor-Green vortex canonical flow. The second case study focuses on the effect of resolution on flow physics and loss generation and uses a compressor cascade subjected to freestream turbulence. The results show that both resolving local entropy generation rate and capturing the inception and growth of instabilities are critical to accuracy of loss prediction. In particular, the interaction of free-stream turbulence at the leading-edge and development of instabilities in the laminar region of the boundary layer are critical to capturing loss.
publisherThe American Society of Mechanical Engineers (ASME)
titleAccurate Prediction of Loss Using High Fidelity Methods
typeJournal Paper
journal volume143
journal issue3
journal titleJournal of Turbomachinery
identifier doi10.1115/1.4050115
journal fristpage031008-1
journal lastpage031008-9
page9
treeJournal of Turbomachinery:;2021:;volume( 143 ):;issue: 003
contenttypeFulltext


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