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Experimental Investigation of Heat Transfer in a Rotor-Stator Cavity with Cooling Air Inlet at Low Radius. / Luo, X; Wang, L; Zhao, X; Xu, G; Wu, Hongwei.

In: International Journal of Heat and Mass Transfer, Vol. 76, 30.09.2014, p. 65-80.

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@article{b939675eb0b440fd85963d22cdb8a91b,
title = "Experimental Investigation of Heat Transfer in a Rotor-Stator Cavity with Cooling Air Inlet at Low Radius",
abstract = "This article presents an experimental investigation of the heat transfer characteristics in a typical rotor–stator system with cooling air inlet at low radius under different dimensionless flow rate (CW) ranges from 1.32 × 104 to 4.87 × 104 at five different rotational speeds, i.e., 500, 1000, 1500, 2000 and 2500 rpm with a large range of rotational Reynolds numbers 4.18 × 105 ⩽ Reω ⩽ 2.484 × 106. A transient thermochromic liquid crystal (TLC) technique is employed to obtain the detailed distribution of the Nusselt number (Nu) on the surface of the rotor with effective rotating radius of 350 mm as well as with a maximum gap of 67 mm between the rotor and stator. The relationship between the Nusselt number (Nu) and the turbulent flow parameter (λT) which has been identified as the parameter governing heat transfer in the rotating disk system is experimentally explored. A numerical model is developed for the investigation of the flow structure inside the rotating cavity and provides a basis for further study in explaining the heat transfer behavior over the rotating disk. It is found that the heat transfer characteristics are strongly affected by the flow structure. Numerical results also clearly show the existence of three flow regimes inside the cavity, namely, viscous regime, co-dominated regime, and inertial regime. The heat transfer characteristics in a rotor–stator system are well explained by the flow structure obtained in the paper.",
author = "X Luo and L Wang and X Zhao and G Xu and Hongwei Wu",
note = "X. Luo, L. Wang, X. Zhao, G. Xu, and H. Wu, 'Experimental investigation of heat transfer in a rotor–stator cavity with cooling air inlet at low radius', International Journal or Heat and Mass Transfer, Vol. 76, pp. 65-80, May 2014, doi: https://doi.org/10.1016/j.ijheatmasstransfer.2014.04.013. Published by Elsevier. Copyright {\circledC} 2014 Elsevier Ltd. All rights reserved.",
year = "2014",
month = "9",
day = "30",
doi = "10.1016/j.ijheatmasstransfer.2014.04.013",
language = "English",
volume = "76",
pages = "65--80",
journal = "International Journal of Heat and Mass Transfer",
issn = "0017-9310",
publisher = "Elsevier Limited",

}

RIS

TY - JOUR

T1 - Experimental Investigation of Heat Transfer in a Rotor-Stator Cavity with Cooling Air Inlet at Low Radius

AU - Luo, X

AU - Wang, L

AU - Zhao, X

AU - Xu, G

AU - Wu, Hongwei

N1 - X. Luo, L. Wang, X. Zhao, G. Xu, and H. Wu, 'Experimental investigation of heat transfer in a rotor–stator cavity with cooling air inlet at low radius', International Journal or Heat and Mass Transfer, Vol. 76, pp. 65-80, May 2014, doi: https://doi.org/10.1016/j.ijheatmasstransfer.2014.04.013. Published by Elsevier. Copyright © 2014 Elsevier Ltd. All rights reserved.

PY - 2014/9/30

Y1 - 2014/9/30

N2 - This article presents an experimental investigation of the heat transfer characteristics in a typical rotor–stator system with cooling air inlet at low radius under different dimensionless flow rate (CW) ranges from 1.32 × 104 to 4.87 × 104 at five different rotational speeds, i.e., 500, 1000, 1500, 2000 and 2500 rpm with a large range of rotational Reynolds numbers 4.18 × 105 ⩽ Reω ⩽ 2.484 × 106. A transient thermochromic liquid crystal (TLC) technique is employed to obtain the detailed distribution of the Nusselt number (Nu) on the surface of the rotor with effective rotating radius of 350 mm as well as with a maximum gap of 67 mm between the rotor and stator. The relationship between the Nusselt number (Nu) and the turbulent flow parameter (λT) which has been identified as the parameter governing heat transfer in the rotating disk system is experimentally explored. A numerical model is developed for the investigation of the flow structure inside the rotating cavity and provides a basis for further study in explaining the heat transfer behavior over the rotating disk. It is found that the heat transfer characteristics are strongly affected by the flow structure. Numerical results also clearly show the existence of three flow regimes inside the cavity, namely, viscous regime, co-dominated regime, and inertial regime. The heat transfer characteristics in a rotor–stator system are well explained by the flow structure obtained in the paper.

AB - This article presents an experimental investigation of the heat transfer characteristics in a typical rotor–stator system with cooling air inlet at low radius under different dimensionless flow rate (CW) ranges from 1.32 × 104 to 4.87 × 104 at five different rotational speeds, i.e., 500, 1000, 1500, 2000 and 2500 rpm with a large range of rotational Reynolds numbers 4.18 × 105 ⩽ Reω ⩽ 2.484 × 106. A transient thermochromic liquid crystal (TLC) technique is employed to obtain the detailed distribution of the Nusselt number (Nu) on the surface of the rotor with effective rotating radius of 350 mm as well as with a maximum gap of 67 mm between the rotor and stator. The relationship between the Nusselt number (Nu) and the turbulent flow parameter (λT) which has been identified as the parameter governing heat transfer in the rotating disk system is experimentally explored. A numerical model is developed for the investigation of the flow structure inside the rotating cavity and provides a basis for further study in explaining the heat transfer behavior over the rotating disk. It is found that the heat transfer characteristics are strongly affected by the flow structure. Numerical results also clearly show the existence of three flow regimes inside the cavity, namely, viscous regime, co-dominated regime, and inertial regime. The heat transfer characteristics in a rotor–stator system are well explained by the flow structure obtained in the paper.

U2 - 10.1016/j.ijheatmasstransfer.2014.04.013

DO - 10.1016/j.ijheatmasstransfer.2014.04.013

M3 - Article

VL - 76

SP - 65

EP - 80

JO - International Journal of Heat and Mass Transfer

JF - International Journal of Heat and Mass Transfer

SN - 0017-9310

ER -