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Low-Reynolds Mathematical Modeling of the
Structure of Vortex Zones Between Periodic
Surface-Located Flow Turbulators of Semicircular
Cross-Section in Pipes
Lobanov IE*
Doctor of Technical Sciences, Moscow
Annotation
Mathematical modeling of the structure of vortex zones between periodic surface-located
flow turbulators of a semicircular and square cross-section is carried out on the basis of
multi-block computational technologies based on the solution of the factorized finite-volume
method of the Reynolds equations (closed with the help of the Menter shear stress transfer
mode) and the energy equation (on different-scale intersecting structured grids). This method
was previously successfully applied and verified by experiment. An exhaustive analysis of the
corresponding streamlines is presented, proving the advantage of abruded turbulators.
A well-known and very well-tested in practice method of vortex intensification of heat
transfer is the application of periodic protrusions on the walls of the washed surfaces [1]. The
study of the structure of the intensified flow is mainly carried out by experimental methods
[1], while modern computational works on this topic are relatively few [2] and are only
partially devoted directly to the structure of the intensified flow; some of the methods (for
example, a certain part of works [2]) use only integral approaches to this problem. This work
is directly devoted to the study of the flow structure in the pipe, For pipes with turbulators of a
semicircular cross-section, the nature of the relationship between heat transfer and hydraulic
resistance remains similar to the above-considered nature of the relationship for square flow
turbulators, but the values (Nu/Nusm)/(/sm) for the former, as a rule, is definitely higher
due to the much smaller influence of the systems of secondary and corner vortices, which
occurs due to deformation and greater elongation of the main vortex, which is confirmed
by the corresponding values for pipes with turbulators of a semicircular cross-section (Nu/
Nusm) / (/sm)=0.89 for t/D = 1.00, d/D=0.94, Re=104; (Nu/Nusm)/(/sm)=0.68 for
d/D=0.94, t/D=0.50, Re=104; (Nu/Nusm) / (/sm)=0.80 for d/D=0.94, t/D=0.25, Re=104.
Similar conclusions will take place at higher relative heights of turbulators (at d/D=0.90),
but at lower values of the complex (Nu/Nusm)/(/sm). For example, for turbulators
with a semicircular cross-section, this complex in the considered range of determining
parameters (d/D = 0.90; t/D = 0.25÷1.00; Re = = 104 ÷ 105) is of the order of (Nu/Nusm)/
(/sm=0.31÷0.50.
For square turbulators, the above complex is even smaller. The structure of the vortex
zones before and after the rib largely depends on its geometry and the coolant flow regime.
The prevalence of the generation of turbulence over dissipation occurs mainly at the
boundary of the vortex zone remote from the wall, where the velocity gradient, as well as
turbulent stresses, are maximum. When intensifying heat transfer by turbulators of square
Crimson Publishers
Wings to the Research
Opinion
*Corresponding author: Lobanov IE,
Doctor of Technical Sciences, Moscow
Submission: November 20, 2020
Published: December 09, 2020
Volume 4 - Issue 1
How to cite this article: Lobanov IE.
Low-Reynolds Mathematical Modeling
of the Structure of Vortex Zones
Between Periodic Surface-Located
Flow Turbulators of Semicircular
Cross-Section in Pipes. Surg Med Open
Acc J. 4(1). SMOAJ.000579. 2020.
DOI: 10.31031/SMOAJ.2020.04.000579
Copyright@ Lobanov IE, This article is
distributed under the terms of the Creative
Commons Attribution 4.0 International
License, which permits unrestricted use
and redistribution provided that the
original author and source are credited.
ISSN: 2578-0379
1
Surgical Medicine Open Access Journal
2
Surg Med Open Acc J Copyright © Lobanov IE
SMOAJ.MS.ID.000579. 4(1).2020
cross section, i.e. rather sharp outlines, the energy dissipation
that occurs in powerful vortices before and behind them can be
comparable to the development of turbulence in them (except
for the upper edge of the turbulator), which causes increased
hydraulic losses. For pipes with turbulators with a semicircular
cross-section, i.e. rather smooth outlines, the above effect is largely
neutralized. Consequently, it is more optimal to switch to abruted
turbulators (the maximum generation of turbulence in them is
located approximately at the level of the upper boundary of the
protrusion), where the hydraulic losses are much less, which is
confirmed by experimental data.
References
1.	 Kalinin EK, Dreitser GA, Kopp IZ (1998) Effective surfaces of heat
exchange. Energoatomizdat, p.408.
2.	 Lobanov IE, NV Paramonov (2011) Mathematical modeling of intensified
heat transfer during flow in channels on the basis of complex models of a
turbulent boundary layer. Publishing house MAI, p.160.
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Smoaj.000579

  • 1. Low-Reynolds Mathematical Modeling of the Structure of Vortex Zones Between Periodic Surface-Located Flow Turbulators of Semicircular Cross-Section in Pipes Lobanov IE* Doctor of Technical Sciences, Moscow Annotation Mathematical modeling of the structure of vortex zones between periodic surface-located flow turbulators of a semicircular and square cross-section is carried out on the basis of multi-block computational technologies based on the solution of the factorized finite-volume method of the Reynolds equations (closed with the help of the Menter shear stress transfer mode) and the energy equation (on different-scale intersecting structured grids). This method was previously successfully applied and verified by experiment. An exhaustive analysis of the corresponding streamlines is presented, proving the advantage of abruded turbulators. A well-known and very well-tested in practice method of vortex intensification of heat transfer is the application of periodic protrusions on the walls of the washed surfaces [1]. The study of the structure of the intensified flow is mainly carried out by experimental methods [1], while modern computational works on this topic are relatively few [2] and are only partially devoted directly to the structure of the intensified flow; some of the methods (for example, a certain part of works [2]) use only integral approaches to this problem. This work is directly devoted to the study of the flow structure in the pipe, For pipes with turbulators of a semicircular cross-section, the nature of the relationship between heat transfer and hydraulic resistance remains similar to the above-considered nature of the relationship for square flow turbulators, but the values (Nu/Nusm)/(/sm) for the former, as a rule, is definitely higher due to the much smaller influence of the systems of secondary and corner vortices, which occurs due to deformation and greater elongation of the main vortex, which is confirmed by the corresponding values for pipes with turbulators of a semicircular cross-section (Nu/ Nusm) / (/sm)=0.89 for t/D = 1.00, d/D=0.94, Re=104; (Nu/Nusm)/(/sm)=0.68 for d/D=0.94, t/D=0.50, Re=104; (Nu/Nusm) / (/sm)=0.80 for d/D=0.94, t/D=0.25, Re=104. Similar conclusions will take place at higher relative heights of turbulators (at d/D=0.90), but at lower values of the complex (Nu/Nusm)/(/sm). For example, for turbulators with a semicircular cross-section, this complex in the considered range of determining parameters (d/D = 0.90; t/D = 0.25÷1.00; Re = = 104 ÷ 105) is of the order of (Nu/Nusm)/ (/sm=0.31÷0.50. For square turbulators, the above complex is even smaller. The structure of the vortex zones before and after the rib largely depends on its geometry and the coolant flow regime. The prevalence of the generation of turbulence over dissipation occurs mainly at the boundary of the vortex zone remote from the wall, where the velocity gradient, as well as turbulent stresses, are maximum. When intensifying heat transfer by turbulators of square Crimson Publishers Wings to the Research Opinion *Corresponding author: Lobanov IE, Doctor of Technical Sciences, Moscow Submission: November 20, 2020 Published: December 09, 2020 Volume 4 - Issue 1 How to cite this article: Lobanov IE. Low-Reynolds Mathematical Modeling of the Structure of Vortex Zones Between Periodic Surface-Located Flow Turbulators of Semicircular Cross-Section in Pipes. Surg Med Open Acc J. 4(1). SMOAJ.000579. 2020. DOI: 10.31031/SMOAJ.2020.04.000579 Copyright@ Lobanov IE, This article is distributed under the terms of the Creative Commons Attribution 4.0 International License, which permits unrestricted use and redistribution provided that the original author and source are credited. ISSN: 2578-0379 1 Surgical Medicine Open Access Journal
  • 2. 2 Surg Med Open Acc J Copyright © Lobanov IE SMOAJ.MS.ID.000579. 4(1).2020 cross section, i.e. rather sharp outlines, the energy dissipation that occurs in powerful vortices before and behind them can be comparable to the development of turbulence in them (except for the upper edge of the turbulator), which causes increased hydraulic losses. For pipes with turbulators with a semicircular cross-section, i.e. rather smooth outlines, the above effect is largely neutralized. Consequently, it is more optimal to switch to abruted turbulators (the maximum generation of turbulence in them is located approximately at the level of the upper boundary of the protrusion), where the hydraulic losses are much less, which is confirmed by experimental data. References 1. Kalinin EK, Dreitser GA, Kopp IZ (1998) Effective surfaces of heat exchange. Energoatomizdat, p.408. 2. Lobanov IE, NV Paramonov (2011) Mathematical modeling of intensified heat transfer during flow in channels on the basis of complex models of a turbulent boundary layer. Publishing house MAI, p.160. For possible submissions Click below: Submit Article