Influence of turbulence parameters on flow characteristics of cavity with tubed vortex reducer

Yang BAI; Xiang LUO; Jian HE

doi:10.13224/j.cnki.jasp.20210022

Chinese

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Influence of turbulence parameters on flow characteristics of cavity with tubed vortex reducer

Combustion,Heat and Mass Transfer | 更新时间：2025-04-07

- Influence of turbulence parameters on flow characteristics of cavity with tubed vortex reducer
- Journal of Aerospace Power Vol. 37, Issue 6, Pages: 1295-1305(2022)
- 作者机构：
  
  1.北京航空航天大学航空发动机研究院，北京 102206
  2.北京航空航天大学能源与动力工程学院航空发动机气动热力国家级重点实验室，北京 102206
- 作者简介：
- 基金信息：
- DOI：10.13224/j.cnki.jasp.20210022
  CLC：
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Yang BAI, Xiang LUO, Jian HE. Influence of turbulence parameters on flow characteristics of cavity with tubed vortex reducer[J]. Journal of Aerospace Power, 2022, 37(6): 1295-1305.
DOI：

Yang BAI, Xiang LUO, Jian HE. Influence of turbulence parameters on flow characteristics of cavity with tubed vortex reducer[J]. Journal of Aerospace Power, 2022, 37(6): 1295-1305. DOI： 10.13224/j.cnki.jasp.20210022.

摘要

通过计算卷吸流量对传统湍流参数定义进行修正，并验证了修正后的湍流参数对气流流动的控制情况。结果表明：修正后的湍流参数在不同的管氏减涡器进出口位置和入口预旋下均对盘腔内的气流流场和总压系数取得了很好的控制效果。气流总压系数和实际旋流系数均同时受修正湍流参数和入口旋流系数控制。此外，随同转速下的湍流参数增加，气流保持其径向内流状态的能力增强，需要管氏减涡器抑制其周向旋转的区域减少，使得总压系数最小的最优管氏减涡器长度减短。

Abstract

This parameter was modified by calculating the entrainment flow rate.The result showed that the modified turbulence parameter had great control effect on flow state and total pressure coefficient.Both the total pressure coefficient and the effective swirl fraction relied on the modified turbulence parameter and the inlet pre⁃swirl fraction.In addition，the ability of air to maintain radial internal flow state was enhanced with the increase of modified turbulence parameter.Therefore，the area requiring suppress circumferential rotation decreased，which shortened the optimal length of the tubed vortex reducer with the minimum total pressure coefficient.

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references

HIDE R . On source⁃sink flows in a rotating fluid [J]. Journal of Fluid Mechanics Digital Archive , 1968 , 32 （ 4 ）: 737 ⁃ 749 .

BARCILON V . Some inertial modifications of the linear viscous theory of steady rotating fluid flows [J]. Physics of Fluids , 1970 , 13 （ 3 ）: 537 ⁃ 544 .

BENNETTS D A , HOCKING L M . On nonlinear ekman and stewartson layers in a rotating fluid [J]. Proceedings of the Royal Society A:Mathematical,Physical and Engineering Sciences , 1973 , 333 （ 1595 ）: 469 ⁃ 489 .

BENNETTS D A , JACKSON W D N . Source–sink flows in a rotating annulus:a combined laboratory and numerical study [J]. Journal of Fluid Mechanics , 1974 , 66 （ 4 ）: 689 ⁃ 705 .

OWEN J M , PINCOMBE J R , ROGERS R H . Source⁃sink flow inside a rotating cylindrical cavity [J]. Journal of Fluid Mechanics , 1985 , 155 : 233 ⁃ 265 .

FIROUZIAN M , OWEN J M , PINCOMBE J R , et al . Flow and heat transfer in a rotating cavity with a radial inflow of fluid:Part 1 the flow structure [J]. International Journal of Heat and Fluid Flow , 1985 , 6 （ 4 ）: 228 ⁃ 234 .

于霄 , 罗翔 , 徐国强 , 等 . 用PIV技术测量径向进气旋转盘腔内的流动 [J]. 航空动力学报 , 2009 , 24 （ 11 ）: 2483 ⁃ 2488

YU Xiao , LUO Xiang , XU Guoqiang , et al . Particle image velocimetry （PIV） measurements of the flow in a rotating cavity with a radial inflow [J]. Journal of Aerospace Power , 2009 , 24 （ 11 ）: 2483 ⁃ 2488 . （in Chinese）

冯安 . 径向入流旋转盘腔减涡器减阻特性研究 [D]. 北京：北京航空航天大学， 2015 .

FENG An,Investigation on varied vortex reducers in reducing the pressure drop in a rotating cavity with radial inflow [D]. Beijing : Beihang University , 2015 . （in Chinese）

FIROUZIAN M , OWEN J M , PINCOMBE J R , et al . Flow and heat transfer in a rotating cylindrical cavity with a radial inflow of fluid:Part 2 velocity,pressure and heat transfer measurements [J]. International Journal of Heat and Fluid Flow , 1986 , 7 （ 1 ）: 21 ⁃ 27 .

FARTHING P R , OWEN J M . De⁃swirled radial inflow in a rotating cavity [J]. International Journal of Heat and Fluid Flow , 1991 , 12 （ 1 ）: 63 ⁃ 70 .

MIRZAEE I , GAN X , WILSON M , et al . Heat transfer in a rotating cavity with a peripheral inflow and outflow of cooling air [J]. Journal of Turbomachinery , 1998 , 120 （ 4 ）: 818 ⁃ 823 .

JAAFAR A A , MOTALLEBI F , WILSON M , et al . Flow and heat transfer in a rotating cavity with a stationary stepped casing [R]. ASME Paper GT2000⁃281 , 2000 .

蔡旭 . 复杂进口条件下旋转盘腔流动和换热研究 [D]. 北京 : 北京航空航天大学 , 2014 .

CAI Xu，Study on fluid flow and heat transfer in rotating cavities with complex inlet conditions [D]. Beijing : Beihang University , 2014 . （in Chinese）

赵熙 . 复杂涡轮盘腔内流动与换热研究 [D]. 北京 : 北京航空航天大学 , 2012 .

ZHAO Xi . Study on fluid flow and heat transfer in rotor⁃stator turbine disc cavities with complex boundary conditions [D]. Beijing : Beihang University , 2012 . （in Chinese）

赵秋月 , 娄德仓 , 郭文 , 等 . 旋转盘腔去旋系统数值模拟 [J]. 燃气涡轮试验与研究 , 2014 , 27 （ 5 ）: 43 ⁃ 48 .

ZHAO Qiuyue , LOU Decang , GUO Wen , et al . Numerical simulation for the de⁃swirled system in rotating cavity [J]. Gas Turbine Experiment and Research , 2014 , 27 （ 5 ）: 43 ⁃ 48 . （in Chinese）

LIANG Z R , LUO X , FENG Y , et al . Experimental investigation of pressure losses in a co⁃rotating cavity with radial inflow employing tubed vortex reducers with varied nozzles [J]. Experimental Thermal and Fluid Science , 2015 , 66 : 304 ⁃ 315 .

LUO X , FENG A , QUAN Y , et al . Experimental analysis of varied vortex reducers in reducing the pressure drop in a rotating cavity with radial inflow [J]. Experimental Thermal and Fluid Science , 2016 , 77 : 159 ⁃ 166 .

SIBILLI T , CHO G , KHOLI F , et al . Numerical analysis of industrial gas turbine secondary air systems employing vortex reducers [R]. ASME Paper GT2018⁃76313 , 2018 .

PEITSCH D , STEIN M , HEIN S , et al . Numerical investigation of vortex reducer flows in the high pressure compressor of modern aeroengines [R]. ASME Paper GT2002⁃30674 , 2002 .

白阳 , 罗翔 , 何健 , 等 . 导流板式减涡器总压损失特性数值模拟 [J]. 航空动力学报 , 2019 , 34 （ 10 ）: 2120 ⁃ 2130 .

BAI Yang , LUO Xiang , HE Jian , et al . Numerical study of total pressure loss on vortex⁃reducer with bafflers [J]. Journal of Aerospace Power , 2019 , 34 （ 10 ）: 2120 ⁃ 2130 . （in Chinese）

蔡超凡 . 径向内流减涡器减阻特性数值模拟研究 [D]. 北京：北京航空航天大学， 2018 .

CAI Chaofan . Investigation on numerical simulation of pressure loss characteristics of radial inflow vortex reducer [D]. Beijing : Beihang University , 2018 . （in Chinese）

ANDRÉ G , WIELAND U , ERWIN K , et al . Experimental analysis of varied vortex reducer configurations for the internalair system of jet engine gas turbines [R]. ASME Paper GT2008⁃50738 , 2008 .

田冉冉 , 毛军逵 , 范俊 , 等 . 反旋进气混合式减涡结构流动特性数值计算 [J]. 航空动力学报 , 2019 , 34 （ 8 ）: 1677 ⁃ 1687 .

TIAN Ranran , MAO Junkui , FAN Jun , et al . Numerical calculation of flow characteristics of hybrid vortex reduce structure combing de⁃swirl inlet [J]. Journal of Aerospace Power , 2019 , 34 （ 8 ）: 1677 ⁃ 1687 . （in Chinese）

KUMAR B G V , CHEW J W , HILLS N J . Rotating flow and heat transfer in cylindrical cavities with radial inflow [J]. Journal of Engineering for Gas Turbines & Power , 2013 , 135 （ 3 ）: 2047 ⁃ 2060 .

杜禧 . 径向内流减涡器减阻特性实验研究 [D]. 北京：北京航空航天大学， 2018 .

DU Xi . Investigation on pressure drop of centripetal air⁃bleed system employing tubed vortex reducers [D]. Beijing : Beihang University , 2018 . （in Chinese）

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