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contributor authorVerstraete, Tom
contributor authorColetti, Filippo
contributor authorBulle, Jأ©rأ©my
contributor authorVanderwielen, Timothأ©e
contributor authorArts, Tony
date accessioned2017-05-09T01:03:49Z
date available2017-05-09T01:03:49Z
date issued2013
identifier issn0889-504X
identifier otherturb_135_05_051015.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/153496
description abstractThis twopart paper addresses the design of a Ubend for serpentine internal cooling channels optimized for minimal pressure loss. The total pressure loss for the flow in a Ubend is a critical design parameter, as it augments the pressure required at the inlet of the cooling system, resulting in a lower global efficiency. In this first part of the paper, the design methodology of the cooling channel is presented. The minimization of the total pressure loss is achieved by means of a numerical optimization method that uses a metamodelassisted differential evolution algorithm in combination with an incompressible Navier–Stokes solver. The profiles of the internal and external side of the bend are parameterized using piecewise Bezier curves. This allows for a wide variety of shapes, respecting the manufacturability constraints of the design. The pressure loss is computed by the Navier–Stokes solver, which is based on a twoequation turbulence model and is available from the open source software OpenFOAM. The numerical method predicts an improvement of 36% in total pressure drop with respect to a circular Ubend, mainly due to the reduction of the separated flow region along the internal side of the bend. The resulting design is subjected to experimental validation, presented in Part II of the paper.
publisherThe American Society of Mechanical Engineers (ASME)
titleOptimization of a U Bend for Minimal Pressure Loss in Internal Cooling Channels—Part I: Numerical Method
typeJournal Paper
journal volume135
journal issue5
journal titleJournal of Turbomachinery
identifier doi10.1115/1.4023030
journal fristpage51015
journal lastpage51015
identifier eissn1528-8900
treeJournal of Turbomachinery:;2013:;volume( 135 ):;issue: 005
contenttypeFulltext


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