APPLICATION OF NON-LINEAR COMPACT SCHEMES TO COMPLEX TURBULENCE DIRECT NUMERICAL SIMULATIONS SUCH AS MULTI-PHASE FLOW
APPLICATION OF NON-LINEAR COMPACT SCHEMES TO COMPLEX TURBULENCE DIRECT NUMERICAL SIMULATIONS SUCH AS MULTI-PHASE FLOW
批准号:
13650169
负责人:
MAEKAWA Hiroshi
金额:
$2.3万
依托单位国家:
日本
项目类别:
Grant-in-Aid for Scientific Research (C)
财政年份:
2001
资助国家:
日本
项目状态:
已结题
起止时间:
2001 至 2002
中文摘要
本研究主要研究非线性紧致格式在多相流等复杂湍流问题中的应用。紧致格式在湍流模拟中具有分辨率高、相位误差小等优点。然而,对称紧致格式没有任何非线性处理的应用,几乎没有成功的物理间断的流动,由于计划的色散误差。另一方面,ENO型格式有太大的耗散误差,以解决传播的声波。本项目研究了三个试验问题:(1)高马赫数钝体流动对外部声波的感受性,(2)超声速剪切层的声波发射机理,(3)气泡溃灭和微射流。迎风紧致格式的优点是能在较高波数下求解流场,并能在高波数下产生耗散效应,从而抑制数值振荡。对这些格式的进一步处理,如数值通量的凸组合,被证明能成功地捕捉到大的间断和非常小的声波。
英文摘要
In this research project, application of non-linear compact schemes to simulations of complex turbulence with discontinuities, such as multi-phase flow turbulence, is studied. Compact schemes have a few advantages of high-resolution and minimum phase-error for turbulence simulations. However, application of symmetric compact schemes without any nonlinear treatment to the flow with physical discontinuities has hardly been successful due to the schemes dispersion error. On the other hand, ENO-type schemes have too large dissipation error to resolve propagating acoustic waves. In this project, three test problems have been investigated; (1) High Mach number blunt body flow receptivity to external acoustic waves, (2) Acoustic wave emission mechanism from supersonic shear layer, (3) Bubble collapse and microjet. Upwind compact schemes have an advantage to resolve the flow fields up to rather high-wavenumber and present a dissipation effect to damp numerical oscillation at only high-wavenumbers Advanced treatments of these schemes, such as convex combination of numerical flux, were proved to be successful to capture both large discontinuities and very small acoustic waves, For bubble distortion and breakdown simulations, a non-linear filter technique was employed.
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竹原洋三: "圧縮性乱流DNSを使ったLESモデルの評価と比較"日本流体力学会 年会2002講演論文集. 396-397 (2002)
Yozo Takehara:“使用可压缩湍流 DNS 的 LES 模型的评估和比较”日本流体力学学会 2002 年年会记录 396-397 (2002)。
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M.Yahyaoui: "Direct Numerical Simulations of Subsonic Plane Poiseuille Flows Undergoing Transition"JSME International Journal. 44・1. 72-80 (2001)
M. Yahyaoui:“过渡中的亚音速平面泊肃叶流的直接数值模拟”JSME 国际期刊 44・1(2001 年)。
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H.Maekawa: "Study of Mach Wave Emission Mechanism in a Turbulent Jet at High Convective Mach Numbers Using DNS"Russia-Japan International Workshop on Actual Problems of Computational Mechanics. 招待講演. 32-33 (2002)
H. Maekawa:“使用 DNS 对高对流马赫数湍流射流中的马赫波发射机制进行研究”俄罗斯-日本计算力学实际问题研讨会 32-33 (2002)。
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前川 博: "対話とシミュレーションムービーでまなぶ流体力学"共立出版. 147 (2002)
Hiroshi Maekawa:“通过对话和模拟电影学习流体力学”Kyoritsu Shuppan 147 (2002)。
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渡邊大輔: "DNSによる超音速自由せん断流における音波放出機構の研究"航空宇宙数値シミュレーション技術シンポジウム講演論文集. NAL special Publication SP. 72-77 (2002)
Daisuke Watanabe:“使用 DNS 进行超音速自由剪切流中的声发射机制研究”航空航天数值模拟技术研讨会论文集 NAL 特别出版物 SP。
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共 32 条
Skin-friction reduction for the subsonic turbulent boundary layers
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批准号:24656518
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项目类别:Grant-in-Aid for Challenging Exploratory Research
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资助金额:$2.58万
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财政年份:2012
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负责人:MAEKAWA Hiroshi
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依托单位:
STUDY OF LARGE-SCALE DYNAMICS EMANATED IN COMPLEX TURBUBLENT FLOWS
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批准号:21560165
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项目类别:Grant-in-Aid for Scientific Research (C)
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资助金额:$3.08万
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财政年份:2009
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负责人:MAEKAWA Hiroshi
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依托单位:
Study on free shear layrs control by mians of direct numerical simulations.
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批准号:03650154
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项目类别:Grant-in-Aid for General Scientific Research (C)
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资助金额:$1.41万
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财政年份:1991
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负责人:MAEKAWA Hiroshi
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依托单位: