TY - JOUR
T1 - Optimization of a U-bend for minimal pressure loss in internal cooling channels- part I
T2 - Numerical method
AU - Verstraete, Tom
AU - Coletti, Filippo
AU - Bulle, Jérémy
AU - Vanderwielen, Timothée
AU - Arts, Tony
PY - 2013/6/28
Y1 - 2013/6/28
N2 - This two-part paper addresses the design of a U-bend 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 metamodel-assisted 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 piece-wise 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 two-equation 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 U-bend, 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.
AB - This two-part paper addresses the design of a U-bend 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 metamodel-assisted 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 piece-wise 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 two-equation 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 U-bend, 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.
UR - http://www.scopus.com/inward/record.url?scp=84888033107&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=84888033107&partnerID=8YFLogxK
U2 - 10.1115/1.4023030
DO - 10.1115/1.4023030
M3 - Article
AN - SCOPUS:84888033107
SN - 0889-504X
VL - 135
JO - Journal of Turbomachinery
JF - Journal of Turbomachinery
IS - 3
M1 - 051015
ER -