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作者(中文):陳宇翰
作者(外文):Chen, Yu-Han
論文名稱(中文):多鬆弛時間晶格波茲曼法於圖形顯示卡叢集模擬方管内週期性山坡之二次流動
論文名稱(外文):Simulation of secondary motion in duct with periodic hill via multiple-relaxation time lattice Boltzmann method on multi-GPU cluster
指導教授(中文):林昭安
指導教授(外文):Lin, Chao-An
口試委員(中文):廖川傑
吳毓庭
口試委員(外文):Liao, Chuan-Chieh
Wu, Yu-Ting
學位類別:碩士
校院名稱:國立清華大學
系所名稱:動力機械工程學系
學號:109033703
出版年(民國):111
畢業學年度:110
語文別:英文
論文頁數:63
中文關鍵詞:計算流體力學晶格波茲曼法二次流週期性山坡紊流
外文關鍵詞:computational fluid dynamicsCFDlattice Boltzmann methodsecondary motionperiodic hillturbulence
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對管道中的周期性山丘進行數值模擬,並分析產生二次運動的因素。研究中模擬了 Re = 50、200、220 和 700 的具有周期性山丘的管道中的層流和湍流以及 Re = 50、700 的具有周期性山丘的通道中的層流和湍流。 根據瞬時流向速度的觀測,臨界雷諾數約為Re = 220。根據不同雷諾數下和不同位置二次流的比較,最顯著的變化發生在Y = 2h。 為了闡明二次流的貢獻,使用雷諾平均Navier-Stokes方程將流速分解為黏性、湍流、對流和幾何項。 在
Y = 2h 處截面的分解速度,對流項在上半部和下半部分別為負和正,而幾何項則呈現相反的趨勢。 此外,流項在大多數情況下為負值,粘性項的輪廓與截面形狀有關。對雷諾平均 Navier-Stokes 方程進行積分以獲得摩擦係數和阻力係數。 與局部摩擦係數相關的幾何和對流項表現出相反的趨勢,在山坡上具有極值,尤其是在迎風面。全域阻力係數隨著雷諾數的增加而減小,在相同雷諾數下,渠道流的值略高於管道流的值。
Numerical simulations of periodic hills in a duct are performed to analyze the factors that produce secondary motion. Specifically, laminar and turbulent flow in a duct with periodic hills for Re = 50, 200, 220, and 700 and in a channel with periodic hills for Re = 50, 700 are simulated. According to the observations of the instantaneous streamwise velocity, the critical Reynolds number is approximately Re = 220. According to the comparison of the secondary flow in different locations at different Reynolds numbers, the most notable change occurs at Y = 2h. To clarify the contribution of the secondary flow, the flow velocity is decomposed into viscous, turbulent, convection, and geometric terms by using the Reynolds-averaged Navier–Stokes equation. For the decomposed velocities in the cross-section at Y = 2, the convection term is negative and positive in the upper and lower halves, respectively, whereas the geometric term exhibits the opposite trend. Additionally, the turbulent term is negative in most cases, and the profile of the viscous term is related to the shape of the section. The Reynolds-averaged Navier–Stokes equation is integrated to obtain the friction and drag coefficients. The geometric and convective terms associated with the local friction coefficients exhibit opposing tendencies, with extreme values on the hill, especially on the windward side. The global drag coefficient decreases with increasing Reynolds number, and the value for the channel flow is slightly higher than that for the duct flow at the same Reynolds number.
1 Introduction 1
1.1 Introduction . . . . . . . . . . . . . . . . . . . . . . . . . . 1
1.2 Literature survey . . . . . . . . . . . . . . . . . . . . . . . 2
1.2.1 Theory of LBM . . . . . . . . . . . . . . . . . . . . . . . . 2
1.2.2 Flow over periodic hills . . . . . . . . . . . . . . . . . . . 3
1.2.3 Secondary flow . . . . . . . . . . . . . . . . . . . . . . . . 3
1.2.4 Boundary conditions . . . . . . . . . . . . . . . . . . . . . 4
1.2.5 GPU implementation . . . . . . . . . . . . . . . . . . . . . . 5
1.3 Motivation . . . . . . . . . . . . . . . . . . . . . . . . . . . 6
2 Methodology 8
2.1 The Boltzmann equation . . . . . . . . . . . . . . . . . . . . . 8
2.1.1 Basic assumptions . . . . . . . . . . . . . . . . . . . . . . .8
2.1.2 The BGK approximation . . . . . . . . . . . . . . . . . . . . 9
2.1.3 The low-Mach-number approximation . . . . . . . . . . . . . . 11
2.2 Discretization of Boltzmann equation . . . . . . . . . . . . . .12
2.2.1 Discretization of time . . . . . . . . . . . . . . . . . . . .12
2.2.2 Discretization of phase space . . . . . . . . . . . . . . . . 13
3 Numerical algorithm 15
3.1 Multiple-relaxation-time lattice Boltzmann method . . . . . . . 15
3.2 Forcing term . . . . . . . . . . . . . . . . . . . . . . . . . .19
3.3 Boundary conditions . . . . . . . . . . . . . . . . . . . . . . 20
3.3.1 Halfway bounce-back boundary condition . . . . . . . . . . . .20
3.3.2 BFL scheme . . . . . . . . . . . . . . . . . . . . . . . . . .21
3.4 GPU implementation . . . . . . . . . . . . . . . . . . . . . . .23
4 Numerical results and discussion 26
4.1 The geometry of periodic hill . . . . . . . . . . . . . . . . . 26
4.2 The flow over the periodic hill in the channel . . . . . . . . .29
4.2.1 Variables in main flow direction . . . . . . . . . . . . . . .29
4.3 The flow over the periodic hill in the duct . . . . . . . . . . 33
4.3.1 The flow field of the periodic hill in the duct . . . . . . . 33
4.3.2 Critical Reynolds number . . . . . . . . . . . . . . . . . . .33
4.3.3 Comparison of the secondary flow of the periodic hill flow . .34
4.4 The role of secondary motions . . . . . . . . . . . . . . . . . 41
4.4.1 Contributions to streamwise velocity . . . . . . . . . . . . .41
4.4.2 Contributions to the friction coefficient . . . . . . . . . . 42
5 Conclusion and Future work 54
5.1 Conclusion . . . . . . . . . . . . . . . . . . . . . . . . . . .54
5.2 Future work . . . . . . . . . . . . . . . . . . . . . . . . . . 55
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