Effects of Surface Roughness on Windage Loss and Flow Characteristics in Shaft-Type Gap with Critical CO<sub>2</sub>

To investigate the effects of surface roughness on windage loss and flow characteristics in a shaft-type gap, the skin friction coefficient (<i>C</i><sub>f</sub>) and flow versus Reynolds number (<i>Re</i>) at different surface roughness (<i>Ra</i>) an...

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Main Authors: Lehao Hu, Qinghua Deng, Zhouyang Liu, Jun Li, Zhenping Feng
Format: Article
Language:English
Published: MDPI AG 2022-12-01
Series:Applied Sciences
Subjects:
Online Access:https://www.mdpi.com/2076-3417/12/24/12631
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author Lehao Hu
Qinghua Deng
Zhouyang Liu
Jun Li
Zhenping Feng
author_facet Lehao Hu
Qinghua Deng
Zhouyang Liu
Jun Li
Zhenping Feng
author_sort Lehao Hu
collection DOAJ
description To investigate the effects of surface roughness on windage loss and flow characteristics in a shaft-type gap, the skin friction coefficient (<i>C</i><sub>f</sub>) and flow versus Reynolds number (<i>Re</i>) at different surface roughness (<i>Ra</i>) and radius ratio (<i>η</i>) values were investigated. The results showed that <i>C</i><sub>f</sub> decreased as <i>Re</i> increased, and the rate of decrease was constant at low <i>Re</i> but reduced at high <i>Re</i>. The growing relative deviations between the coefficients of smooth and rough walls with <i>Ra</i> indicated that <i>C</i><sub>f</sub> was influenced by rough walls when <i>Re</i> > 10<sup>2</sup>. Moreover, <i>C</i><sub>f</sub> and the variation rate increased with <i>η</i> and were easily influenced by <i>Ra</i> for larger <i>η</i> at low <i>Re</i>, since the interaction between wall roughness and fluid influences windage loss. In addition, the flow field implied the flow had transitioned to Taylor-Couette flow, Taylor vortexes occurred when <i>Re</i> > 10<sup>2</sup>, and the number of vortexes increased with increasing <i>Ra</i> and were reduced with increasing <i>η</i>. The velocity was divided into three regions and the pressure rose from the rotational to stationary walls, but decreased with growing <i>η</i> as a whole. This paper improves the research exploring windage loss and will help design smaller supercritical CO<sub>2</sub> power devices.
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spelling doaj.art-0d04f9354cf24784b4779d2d1be225512023-11-24T13:01:58ZengMDPI AGApplied Sciences2076-34172022-12-0112241263110.3390/app122412631Effects of Surface Roughness on Windage Loss and Flow Characteristics in Shaft-Type Gap with Critical CO<sub>2</sub>Lehao Hu0Qinghua Deng1Zhouyang Liu2Jun Li3Zhenping Feng4Shaanxi Engineering Laboratory of Turbomachinery and Power Equipment, Institute of Turbomachinery, School of Energy and Power Engineering, Xi’an Jiaotong University, Xi’an 710049, ChinaShaanxi Engineering Laboratory of Turbomachinery and Power Equipment, Institute of Turbomachinery, School of Energy and Power Engineering, Xi’an Jiaotong University, Xi’an 710049, ChinaShaanxi Engineering Laboratory of Turbomachinery and Power Equipment, Institute of Turbomachinery, School of Energy and Power Engineering, Xi’an Jiaotong University, Xi’an 710049, ChinaShaanxi Engineering Laboratory of Turbomachinery and Power Equipment, Institute of Turbomachinery, School of Energy and Power Engineering, Xi’an Jiaotong University, Xi’an 710049, ChinaShaanxi Engineering Laboratory of Turbomachinery and Power Equipment, Institute of Turbomachinery, School of Energy and Power Engineering, Xi’an Jiaotong University, Xi’an 710049, ChinaTo investigate the effects of surface roughness on windage loss and flow characteristics in a shaft-type gap, the skin friction coefficient (<i>C</i><sub>f</sub>) and flow versus Reynolds number (<i>Re</i>) at different surface roughness (<i>Ra</i>) and radius ratio (<i>η</i>) values were investigated. The results showed that <i>C</i><sub>f</sub> decreased as <i>Re</i> increased, and the rate of decrease was constant at low <i>Re</i> but reduced at high <i>Re</i>. The growing relative deviations between the coefficients of smooth and rough walls with <i>Ra</i> indicated that <i>C</i><sub>f</sub> was influenced by rough walls when <i>Re</i> > 10<sup>2</sup>. Moreover, <i>C</i><sub>f</sub> and the variation rate increased with <i>η</i> and were easily influenced by <i>Ra</i> for larger <i>η</i> at low <i>Re</i>, since the interaction between wall roughness and fluid influences windage loss. In addition, the flow field implied the flow had transitioned to Taylor-Couette flow, Taylor vortexes occurred when <i>Re</i> > 10<sup>2</sup>, and the number of vortexes increased with increasing <i>Ra</i> and were reduced with increasing <i>η</i>. The velocity was divided into three regions and the pressure rose from the rotational to stationary walls, but decreased with growing <i>η</i> as a whole. This paper improves the research exploring windage loss and will help design smaller supercritical CO<sub>2</sub> power devices.https://www.mdpi.com/2076-3417/12/24/12631windage lossskin friction coefficientTaylor vortexsurface roughness
spellingShingle Lehao Hu
Qinghua Deng
Zhouyang Liu
Jun Li
Zhenping Feng
Effects of Surface Roughness on Windage Loss and Flow Characteristics in Shaft-Type Gap with Critical CO<sub>2</sub>
Applied Sciences
windage loss
skin friction coefficient
Taylor vortex
surface roughness
title Effects of Surface Roughness on Windage Loss and Flow Characteristics in Shaft-Type Gap with Critical CO<sub>2</sub>
title_full Effects of Surface Roughness on Windage Loss and Flow Characteristics in Shaft-Type Gap with Critical CO<sub>2</sub>
title_fullStr Effects of Surface Roughness on Windage Loss and Flow Characteristics in Shaft-Type Gap with Critical CO<sub>2</sub>
title_full_unstemmed Effects of Surface Roughness on Windage Loss and Flow Characteristics in Shaft-Type Gap with Critical CO<sub>2</sub>
title_short Effects of Surface Roughness on Windage Loss and Flow Characteristics in Shaft-Type Gap with Critical CO<sub>2</sub>
title_sort effects of surface roughness on windage loss and flow characteristics in shaft type gap with critical co sub 2 sub
topic windage loss
skin friction coefficient
Taylor vortex
surface roughness
url https://www.mdpi.com/2076-3417/12/24/12631
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