TY - GEN
T1 - Optimization of a U-bend for minimal pressure loss in internal cooling channels - Part I
T2 - ASME 2011 Turbo Expo: Turbine Technical Conference and Exposition, GT2011
AU - Verstraete, Tom
AU - Coletti, Filippo
AU - Bulle, Jérémy
AU - Vanderwielen, Timothée
AU - Arts, Tony
PY - 2011
Y1 - 2011
N2 - This two-parts 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 U-bend 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 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 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-parts 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 U-bend 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 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 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=84865524133&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=84865524133&partnerID=8YFLogxK
U2 - 10.1115/GT2011-46541
DO - 10.1115/GT2011-46541
M3 - Conference contribution
AN - SCOPUS:84865524133
SN - 9780791854655
T3 - Proceedings of the ASME Turbo Expo
SP - 1665
EP - 1676
BT - ASME 2011 Turbo Expo
Y2 - 6 June 2011 through 10 June 2011
ER -