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contributor authorJefferson
contributor authorTucker, Paul G.
contributor authorNorthall, John D.
contributor authorNagabhushana Rao, V.
date accessioned2017-05-09T01:03:09Z
date available2017-05-09T01:03:09Z
date issued2013
identifier issn0889-504X
identifier otherturb_135_3_031013.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/153334
description abstractA Hamilton–Jacobi differential equation is used to naturally and smoothly (via Dirichlet boundary conditions) set turbulence length scales in separated flow regions based on traditional expected length scales. Such zones occur for example in rimseals. The approach is investigated using two test cases, flow over a cylinder at a Reynolds number of 140,000 and flow over a rectangular cavity at a Reynolds number of 50,000. The Nee–Kovasznay turbulence model is investigated using this approach. Predicted drag coefficients for the cylinder testcase show significant (15%) improvement over standard steady RANS and are comparable with URANS results. The mean flowfield also shows a significant improvement over URANS. The error in reattachment length is improved by 180% compared with the steady RANS kد‰ model. The wake velocity profile at a location downstream shows improvement and the URANS profile is inaccurate in comparison. For the cavity case, the HJ–NK approach is generally comparable with the other RANS models for measured velocity profiles. Predicted drag coefficients are compared with large eddy simulation. The new approach shows a 20–30% improvement in predicted drag coefficients compared with standard one and two equation RANS models. The shape of the recirculation region within the cavity is also much improved.
publisherThe American Society of Mechanical Engineers (ASME)
titleDifferential Equation Specification of Integral Turbulence Length Scales
typeJournal Paper
journal volume135
journal issue3
journal titleJournal of Turbomachinery
identifier doi10.1115/1.4007479
journal fristpage31013
journal lastpage31013
identifier eissn1528-8900
treeJournal of Turbomachinery:;2013:;volume( 135 ):;issue: 003
contenttypeFulltext


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