TY - GEN
T1 - Three-dimensional fluid-structure interaction numerical simulation of new type vortex generators in smooth wavy fin-and-elliptical tube heat exchanger
AU - Lotfi, Babak
AU - Sundén, Bengt
AU - Wang, Qiuwang
N1 - Publisher Copyright:
© 2021, Begell House Inc. All rights reserved.
PY - 2015
Y1 - 2015
N2 - A three-dimensional numerical fluid-structure interaction (FSI) framework is successfully carried out on mechanical behaviour of new vortex generators (VGs) – rectangular trapezoidal winglet (RTW), angle rectangular winglet (ARW), curved angle rectangular winglet (CARW) – in smooth wavy fin-and-elliptical tube (SWFET) heat exchanger using the ANSYS MFX Multi-field® solver. The purpose of the present study is to provide better understanding of the performance of the vortex generator structures in SWFET heat exchangers associated with the alloy material properties and geometric factors, because change in the flow geometry due to deformation of components affects the flow field and the pressure drop or pumping power in finned tube heat exchangers. The Reynolds-averaged Navier-Stokes (RANS) equations with Shear Stress Transport (SST) k − ω turbulence model are applied for modelling of the turbulent flow in SWFET heat exchanger and the linear elastic Cauchy-Navier model is solved for the structural von Mises stress and elastic strain analysis in the vortex generators region. An arbitrary Lagrangian–Eulerian (ALE) formulation is employed for this FSI application. Three-dimensional FSI numerical results illustrate that the maximum magnitude of von Mises stress and elastic strain occurs at the root of the vortex generators and depends on geometrical parameters – geometric shape of VGs, angles of attack (αVG = 15o − 75o ) – and material types. These results reveal that the titanium alloy VGs shows a slightly higher strength and lower elastic strain compared to the aluminium alloy VGs. The lowest values of von Mises stress and elastic strain are obtained for CARW vortex generators and higher values of the von Mises stress and elastic strain occurred for RTW vortex generators, particularly at large attack angles.
AB - A three-dimensional numerical fluid-structure interaction (FSI) framework is successfully carried out on mechanical behaviour of new vortex generators (VGs) – rectangular trapezoidal winglet (RTW), angle rectangular winglet (ARW), curved angle rectangular winglet (CARW) – in smooth wavy fin-and-elliptical tube (SWFET) heat exchanger using the ANSYS MFX Multi-field® solver. The purpose of the present study is to provide better understanding of the performance of the vortex generator structures in SWFET heat exchangers associated with the alloy material properties and geometric factors, because change in the flow geometry due to deformation of components affects the flow field and the pressure drop or pumping power in finned tube heat exchangers. The Reynolds-averaged Navier-Stokes (RANS) equations with Shear Stress Transport (SST) k − ω turbulence model are applied for modelling of the turbulent flow in SWFET heat exchanger and the linear elastic Cauchy-Navier model is solved for the structural von Mises stress and elastic strain analysis in the vortex generators region. An arbitrary Lagrangian–Eulerian (ALE) formulation is employed for this FSI application. Three-dimensional FSI numerical results illustrate that the maximum magnitude of von Mises stress and elastic strain occurs at the root of the vortex generators and depends on geometrical parameters – geometric shape of VGs, angles of attack (αVG = 15o − 75o ) – and material types. These results reveal that the titanium alloy VGs shows a slightly higher strength and lower elastic strain compared to the aluminium alloy VGs. The lowest values of von Mises stress and elastic strain are obtained for CARW vortex generators and higher values of the von Mises stress and elastic strain occurred for RTW vortex generators, particularly at large attack angles.
UR - https://www.scopus.com/pages/publications/85120820994
U2 - 10.1615/ICHMT.2015.IntSympAdvComputHeatTransf.300
DO - 10.1615/ICHMT.2015.IntSympAdvComputHeatTransf.300
M3 - 会议稿件
AN - SCOPUS:85120820994
SN - 9781567004298
T3 - International Symposium on Advances in Computational Heat Transfer
SP - 356
EP - 367
BT - Proceedings of CHT-15
PB - Begell House Inc.
T2 - 6th International Symposium on Advances in Computational Heat Transfer , CHT 2015
Y2 - 25 May 2015 through 29 May 2015
ER -