Flow structure and heat transfer characteristics in rotor-stator cavity with inlet at low radius

X. Luo, X. Zhao, L. Wang, H. Wu, G. Xu

Research output: Contribution to journalArticle

Abstract

In this article, a combined experimental and computational study has been conducted to provide better understanding of the flow structure and heat transfer characteristics in a rotor-stator cavity with inlet at low radius. A new test rig was set up to investigate the heat transfer coefficient using transient thermochromic liquid crystal (TLC) technique. Six different rotational speeds, i.e., 500, 1000, 1500, 2000, 2500, 3000 rpm, were considered. The rotational Reynolds number (Re) is ranging from 4.16 x 10(5) to 2.49 x 10(6), and the flow rate coefficient (C-w) ranges from 1.3 x 10(4) to 4.77 x 10(4), with corresponding turbulent flow parameter (AT) in the range of 0.099 <= lambda(T) <= 1.527. A high-Reynolds-number realizable k-epsilon turbulence model was employed to simulate the flow and heat transfer characteristics in the cavity. The comparison of the local and the average Nusselt number on the surface of the main disk between the numerical results and the experimental data indicated that: (1) both the rotational Reynolds number (Rem) and a newly proposed flow pattern parameter (lambda(TX) = CwRew-1.2) dominated the flow characteristics in the rotor-stator cavity, (2) three different regimes could be determined based on the proposed turbulent flow parameter, namely, viscous regime for lambda(TX) <= 0.0009, co-determined regime for 0.0009 < lambda(TX) < 0.0028, and inertial regime for lambda(TX) >= 0.0028, and (3) the flow structure played an important role in determining the heat transfer performance inside the cavity.
Original languageEnglish
Pages (from-to)291-306
JournalApplied Thermal Engineering
Volume70
Issue number1
DOIs
Publication statusPublished - 5 Sep 2014

Keywords

  • Flow structure
  • Heat transfer
  • Rotor-stator
  • Thermochromic liquid crystal
  • Rotational Reynolds number

Cite this

Luo, X. ; Zhao, X. ; Wang, L. ; Wu, H. ; Xu, G. / Flow structure and heat transfer characteristics in rotor-stator cavity with inlet at low radius. In: Applied Thermal Engineering. 2014 ; Vol. 70, No. 1. pp. 291-306.
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author = "X. Luo and X. Zhao and L. Wang and H. Wu and G. Xu",
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Flow structure and heat transfer characteristics in rotor-stator cavity with inlet at low radius. / Luo, X.; Zhao, X.; Wang, L.; Wu, H.; Xu, G.

In: Applied Thermal Engineering, Vol. 70, No. 1, 05.09.2014, p. 291-306.

Research output: Contribution to journalArticle

TY - JOUR

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AU - Luo, X.

AU - Zhao, X.

AU - Wang, L.

AU - Wu, H.

AU - Xu, G.

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N2 - In this article, a combined experimental and computational study has been conducted to provide better understanding of the flow structure and heat transfer characteristics in a rotor-stator cavity with inlet at low radius. A new test rig was set up to investigate the heat transfer coefficient using transient thermochromic liquid crystal (TLC) technique. Six different rotational speeds, i.e., 500, 1000, 1500, 2000, 2500, 3000 rpm, were considered. The rotational Reynolds number (Re) is ranging from 4.16 x 10(5) to 2.49 x 10(6), and the flow rate coefficient (C-w) ranges from 1.3 x 10(4) to 4.77 x 10(4), with corresponding turbulent flow parameter (AT) in the range of 0.099 <= lambda(T) <= 1.527. A high-Reynolds-number realizable k-epsilon turbulence model was employed to simulate the flow and heat transfer characteristics in the cavity. The comparison of the local and the average Nusselt number on the surface of the main disk between the numerical results and the experimental data indicated that: (1) both the rotational Reynolds number (Rem) and a newly proposed flow pattern parameter (lambda(TX) = CwRew-1.2) dominated the flow characteristics in the rotor-stator cavity, (2) three different regimes could be determined based on the proposed turbulent flow parameter, namely, viscous regime for lambda(TX) <= 0.0009, co-determined regime for 0.0009 < lambda(TX) < 0.0028, and inertial regime for lambda(TX) >= 0.0028, and (3) the flow structure played an important role in determining the heat transfer performance inside the cavity.

AB - In this article, a combined experimental and computational study has been conducted to provide better understanding of the flow structure and heat transfer characteristics in a rotor-stator cavity with inlet at low radius. A new test rig was set up to investigate the heat transfer coefficient using transient thermochromic liquid crystal (TLC) technique. Six different rotational speeds, i.e., 500, 1000, 1500, 2000, 2500, 3000 rpm, were considered. The rotational Reynolds number (Re) is ranging from 4.16 x 10(5) to 2.49 x 10(6), and the flow rate coefficient (C-w) ranges from 1.3 x 10(4) to 4.77 x 10(4), with corresponding turbulent flow parameter (AT) in the range of 0.099 <= lambda(T) <= 1.527. A high-Reynolds-number realizable k-epsilon turbulence model was employed to simulate the flow and heat transfer characteristics in the cavity. The comparison of the local and the average Nusselt number on the surface of the main disk between the numerical results and the experimental data indicated that: (1) both the rotational Reynolds number (Rem) and a newly proposed flow pattern parameter (lambda(TX) = CwRew-1.2) dominated the flow characteristics in the rotor-stator cavity, (2) three different regimes could be determined based on the proposed turbulent flow parameter, namely, viscous regime for lambda(TX) <= 0.0009, co-determined regime for 0.0009 < lambda(TX) < 0.0028, and inertial regime for lambda(TX) >= 0.0028, and (3) the flow structure played an important role in determining the heat transfer performance inside the cavity.

KW - Flow structure

KW - Heat transfer

KW - Rotor-stator

KW - Thermochromic liquid crystal

KW - Rotational Reynolds number

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DO - 10.1016/j.applthermaleng.2014.05.006

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EP - 306

JO - Applied Thermal Engineering

JF - Applied Thermal Engineering

SN - 1359-4311

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ER -