• 文献检索
  • 文档翻译
  • 深度研究
  • 学术资讯
  • Suppr Zotero 插件Zotero 插件
  • 邀请有礼
  • 套餐&价格
  • 历史记录
应用&插件
Suppr Zotero 插件Zotero 插件浏览器插件Mac 客户端Windows 客户端微信小程序
定价
高级版会员购买积分包购买API积分包
服务
文献检索文档翻译深度研究API 文档MCP 服务
关于我们
关于 Suppr公司介绍联系我们用户协议隐私条款
关注我们

Suppr 超能文献

核心技术专利:CN118964589B侵权必究
粤ICP备2023148730 号-1Suppr @ 2026

文献检索

告别复杂PubMed语法,用中文像聊天一样搜索,搜遍4000万医学文献。AI智能推荐,让科研检索更轻松。

立即免费搜索

文件翻译

保留排版,准确专业,支持PDF/Word/PPT等文件格式,支持 12+语言互译。

免费翻译文档

深度研究

AI帮你快速写综述,25分钟生成高质量综述,智能提取关键信息,辅助科研写作。

立即免费体验

超临界压力和跨临界温度下二氧化碳的完全可压缩低马赫数模拟

Fully Compressible Low-Mach Number Simulations of Carbon-dioxide at Supercritical Pressures and Trans-critical Temperatures.

作者信息

Sengupta Uttiya, Nemati Hassan, Boersma Bendiks J, Pecnik Rene

机构信息

Department of Process and Energy, Delft University of Technology, Leeghwaterstraat 39, 2628 CB Delft, Netherlands.

出版信息

Flow Turbul Combust. 2017;99(3):909-931. doi: 10.1007/s10494-017-9872-4. Epub 2017 Nov 21.

DOI:10.1007/s10494-017-9872-4
PMID:30069161
原文链接:https://pmc.ncbi.nlm.nih.gov/articles/PMC6044239/
Abstract

This work investigates fully developed turbulent flows of carbon-dioxide close to its vapour-liquid critical point in a channel with a hot and a cold wall. Two direct numerical simulations are performed at low Mach numbers, with the trans-critical transition near the channel centre and the cold wall, respectively. An additional simulation with constant transport properties is used to selectively investigate the effect of the non-linear equation of state on turbulence. Compared to the case where the pseudo-critical transition occurs in the channel center, the case with the pseudo-critical transition close to the cold wall reveals that compressibility effects can exist in the near-wall region even at low Mach numbers. An analysis of the velocity streaks near the hot and the cold walls also indicates a greater degree of streak coherence near the cold wall. A comparison between the constant and variable viscosity cases at the same Reynolds number, Mach number and having the same isothermal wall boundary conditions reveals that variable viscosity increases turbulence near the cold wall and also causes higher velocity gradients near the hot wall. We also show that the extended van Driest transformation results in a better agreement of the velocity profile with the log-law of the wall compared to the standard van Driest transformation. The semi-locally scaled turbulent velocity fluctuations and the turbulent kinetic energy budgets on the hot and the cold sides of the channel collapse on top of each other, thereby establishing the validity of Morkovin's hypothesis.

摘要

本研究探讨了在具有热壁和冷壁的通道中,接近其气液临界点的二氧化碳充分发展的湍流。在低马赫数下进行了两次直接数值模拟,分别在通道中心附近和冷壁附近发生跨临界转变。还进行了一次具有恒定输运特性的模拟,以选择性地研究非线性状态方程对湍流的影响。与伪临界转变发生在通道中心的情况相比,伪临界转变靠近冷壁的情况表明,即使在低马赫数下,近壁区域也可能存在压缩性效应。对热壁和冷壁附近的速度条纹进行分析,也表明冷壁附近的条纹相干程度更高。在相同雷诺数、马赫数且具有相同等温壁边界条件下,对恒定粘度和可变粘度情况进行比较,结果表明可变粘度会增加冷壁附近的湍流,并且在热壁附近会导致更高的速度梯度。我们还表明,与标准的范德瑞斯特变换相比,扩展的范德瑞斯特变换使速度剖面与壁面对数律的一致性更好。通道热侧和冷侧的半局部尺度湍流速度波动和湍动能收支相互重叠,从而证实了莫尔科文假设的有效性。

https://cdn.ncbi.nlm.nih.gov/pmc/blobs/ef47/6044239/8023d64cc52c/10494_2017_9872_Fig12_HTML.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/ef47/6044239/132b89b2e4ed/10494_2017_9872_Fig1_HTML.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/ef47/6044239/ef8f3c355f41/10494_2017_9872_Fig2_HTML.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/ef47/6044239/fe3274eb4aa2/10494_2017_9872_Fig3_HTML.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/ef47/6044239/1da0372aad19/10494_2017_9872_Fig4_HTML.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/ef47/6044239/aaf048010e58/10494_2017_9872_Fig5_HTML.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/ef47/6044239/240792e7054b/10494_2017_9872_Fig6_HTML.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/ef47/6044239/a548cd4be4fd/10494_2017_9872_Fig7_HTML.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/ef47/6044239/72d4de45afac/10494_2017_9872_Fig8_HTML.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/ef47/6044239/24d80b996c7e/10494_2017_9872_Fig9_HTML.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/ef47/6044239/52c2140eb44a/10494_2017_9872_Fig10_HTML.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/ef47/6044239/27a4169b02d4/10494_2017_9872_Fig11_HTML.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/ef47/6044239/8023d64cc52c/10494_2017_9872_Fig12_HTML.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/ef47/6044239/132b89b2e4ed/10494_2017_9872_Fig1_HTML.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/ef47/6044239/ef8f3c355f41/10494_2017_9872_Fig2_HTML.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/ef47/6044239/fe3274eb4aa2/10494_2017_9872_Fig3_HTML.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/ef47/6044239/1da0372aad19/10494_2017_9872_Fig4_HTML.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/ef47/6044239/aaf048010e58/10494_2017_9872_Fig5_HTML.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/ef47/6044239/240792e7054b/10494_2017_9872_Fig6_HTML.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/ef47/6044239/a548cd4be4fd/10494_2017_9872_Fig7_HTML.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/ef47/6044239/72d4de45afac/10494_2017_9872_Fig8_HTML.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/ef47/6044239/24d80b996c7e/10494_2017_9872_Fig9_HTML.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/ef47/6044239/52c2140eb44a/10494_2017_9872_Fig10_HTML.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/ef47/6044239/27a4169b02d4/10494_2017_9872_Fig11_HTML.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/ef47/6044239/8023d64cc52c/10494_2017_9872_Fig12_HTML.jpg

相似文献

1
Fully Compressible Low-Mach Number Simulations of Carbon-dioxide at Supercritical Pressures and Trans-critical Temperatures.超临界压力和跨临界温度下二氧化碳的完全可压缩低马赫数模拟
Flow Turbul Combust. 2017;99(3):909-931. doi: 10.1007/s10494-017-9872-4. Epub 2017 Nov 21.
2
Mach-number-invariant mean-velocity profile of compressible turbulent boundary layers.可压缩湍流边界层的马赫数不变平均速度剖面。
Phys Rev Lett. 2012 Aug 3;109(5):054502. doi: 10.1103/PhysRevLett.109.054502. Epub 2012 Jul 31.
3
Velocity transformation for compressible wall-bounded turbulent flows with and without heat transfer.有传热和无传热情况下可压缩壁面湍流流动的速度变换
Proc Natl Acad Sci U S A. 2021 Aug 24;118(34). doi: 10.1073/pnas.2111144118.
4
Phenomenological and statistical analyses of turbulence in forced convection with temperature-dependent viscosity under non-Boussinesq condition.非布辛涅斯克条件下温度依赖粘性的强制对流中湍流的现象学和统计分析。
Eur Phys J E Soft Matter. 2013 Oct;36(10):120. doi: 10.1140/epje/i2013-13120-2. Epub 2013 Oct 28.
5
Direct Numerical Simulation Database for Hypersonic Turbulent Boundary Layers.高超声速湍流边界层直接数值模拟数据库
AIAA J. 2018 Nov;56(11):4297-4311. doi: 10.2514/1.J057296. Epub 2018 Sep 30.
6
Generalized lattice Boltzmann equation with forcing term for computation of wall-bounded turbulent flows.用于壁面边界湍流流动计算的带强迫项广义格子玻尔兹曼方程。
Phys Rev E Stat Nonlin Soft Matter Phys. 2009 Feb;79(2 Pt 2):026703. doi: 10.1103/PhysRevE.79.026703. Epub 2009 Feb 10.
7
Kinetic and internal energy transfer in implicit large-eddy simulations of forced compressible turbulence.隐式大涡模拟中强迫可压缩湍流的动力学和内能传递。
Phys Rev E. 2019 Oct;100(4-1):043116. doi: 10.1103/PhysRevE.100.043116.
8
Contribution of Reynolds stress distribution to the skin friction in compressible turbulent channel flows.雷诺应力分布对可压缩湍流槽道流中壁面摩擦力的贡献。
Phys Rev E Stat Nonlin Soft Matter Phys. 2009 Mar;79(3 Pt 2):035301. doi: 10.1103/PhysRevE.79.035301. Epub 2009 Mar 3.
9
Contribution of viscous stress work to wall heat flux in compressible turbulent channel flows.粘性应力功对可压缩湍流槽道流壁面热流的贡献。
Phys Rev E. 2020 Oct;102(4-1):043107. doi: 10.1103/PhysRevE.102.043107.
10
Direct Numerical Simulation and Theory of a Wall-Bounded Flow with Zero Skin Friction.零壁面摩擦的壁面流动直接数值模拟与理论
Flow Turbul Combust. 2017 Jul 27;99(3-4):553-564. doi: 10.1007/s10494-017-9834-x.

引用本文的文献

1
Microconfined High-Pressure Transcritical Channel Flow Database: Laminar, Transitional & Turbulent Regimes.微受限高压跨临界通道流数据库:层流、过渡流和湍流状态
Sci Data. 2024 Aug 23;11(1):916. doi: 10.1038/s41597-024-03757-4.
2
A Review of the Complex Flow and Heat Transfer Characteristics in Microchannels.微通道内复杂流动与传热特性综述
Micromachines (Basel). 2023 Jul 19;14(7):1451. doi: 10.3390/mi14071451.