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contributor authorAsif Hoda
contributor authorSumanta Acharya
date accessioned2017-05-09T00:03:38Z
date available2017-05-09T00:03:38Z
date copyrightJuly, 2000
date issued2000
identifier issn0889-504X
identifier otherJOTUEI-28679#558_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/124476
description abstractThis study investigates the performance of several existing turbulence models for the prediction of film coolant jet in a crossflow. Two-equation models employing k–ε and k–ω closures, broadly categorized as high-Reynolds-number formulations, low-Reynolds-number formulations, DNS-based formulation, and nonlinear formulations have been used to simulate the flow. In all, seven different turbulence models have been tested. Predictions with different models have been compared with experimental results of Ajersch et al. (1995) and with each other to critically evaluate model performance. The assessment of models has been done keeping in mind that all models have been formulated for wall-bounded flows and may not be well suited for the jet-in-a-crossflow situation. Close agreement with experimental results was obtained at the jet exit and far downstream of the jet injection region, but all models typically overpredicted the magnitude of the velocities in the wake region behind the jet. The present study clearly underscores the deficiencies of the current models, and demonstrates the need for improvements. [S0889-504X(00)03002-6]
publisherThe American Society of Mechanical Engineers (ASME)
titlePredictions of a Film Coolant Jet in Crossflow With Different Turbulence Models
typeJournal Paper
journal volume122
journal issue3
journal titleJournal of Turbomachinery
identifier doi10.1115/1.1302322
journal fristpage558
journal lastpage569
identifier eissn1528-8900
keywordsFlow (Dynamics)
keywordsTurbulence
keywordsWakes
keywordsMeasurement
keywordsCoolants
keywordsEquations
keywordsGradients
keywordsShear (Mechanics) AND Stress
treeJournal of Turbomachinery:;2000:;volume( 122 ):;issue: 003
contenttypeFulltext


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