本研究為了解決開放性邊界的問題,以吸收性邊界配合修正 LODI 法,以混 合式邊界條件完成在正方形平行平板間自然對流的計算。本研究成功整合了低速 可壓縮流的數值計算方法與開放性邊界條件的應用,發展了幾乎完整涵蓋所有流 體問題的計算方法。本研究的主要貢獻如下:
1. 低速可壓縮流的計算方法:
過去的多利用流體速度將其區分為可壓縮與不可壓縮流,此種方法限制許多 實際的應用,如高溫自然對流、引擎內部流場與聲場的計算等。本研究利用正方 形 平 行 平 板 自 然 對 流 驗 證 計 算 方 法 的 適 用 性 , 且 由 於 溫 差 極 大 , 不 使 用 Boussinesq 假設來完整計算出浮力效應對流體的影響。
2. GPU 高速平行運算:
由於本研究需要大量的計算資源,為了提升效率節省計算時間與資源,利用 GPU 高速平行運算技術取代傳統的 MPI 與 OpenMP 方法,達成使用個人電腦計 算複雜問題的目的。
3. 開放性邊界條件之應用:
本研究以吸收性邊界條件配合修正 LODI 法,成功解決在開放性邊界上,邊 緣與角落造成的數值不穩定現象,並提高吸收性邊界的效率,以之計算出正方形 平行平板間自然對流的現象,並探討不同加熱位置熱傳機制的差異。此外,對於 高雷利數下之自然對流由層流轉變為紊流的不穩定現象也完整的呈現。
綜上所述,本研究所發展之邊界條件與數值方法將可作為各種開放性邊界問 題之基礎並可進而精準解出各種複雜的流體問題。
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參考文獻
[1] K. Khanafer and K. Vafai, Effective boundary conditions for buoyancy-driven flows and heat transfer in fully open-ended two-dimensional enclosures, Int. J. Heat Mass Transfer 45 (2002) 2527-2538.
[2] D. D. Gray and A. Giorgini, The validity of the boussinesq approximation for liquids and gases, Int. J. Heat Mass Transfer 19 (1976) 545-551.
[3] W.R. Briley, H. McDonald, and S. J. Shamroth, At low Mach number Euler formulation and application to time iterative LBI schemes, AIAA 21(10) (1983) 1467-1469.
[4] E. Turkel, Preconditioned methods for solving the incompressible and low speed compressible equations, J. Comput. Phys. 72 (1987) 277-298.
[5] D. Choi and C.L. Merkel, Application of time-iterative schemes to incompressible flow, AIAA. 25(6) (1985) 1518-1524.
[6] D. Choi and C.L. Merkel, The Application of Preconditioning in Viscous Flows, J.
Comput. Phys. 105 (1193) 207-223.
[7] P. L. Roe, Approximation Riemann solver, Parameter Vectors, and Difference Schemes, J. Comput. Phys. 43 (1981) 357-372.
[8] J. M. Weiss and W. A. Simth, Preconditioning Applied to Variable and Constants Density Flows, AIAA. 33 (1995) 2050-2056.
[9] H. Paillere, C. Viozat, A. Kumbaro, and I. Toumi, Comparison of low Mach number models for natural convection problems, Heat and Mass Transfer 36 (2000) 567-573.
[10] D. H. Rudy and J. C. Strikwerda, A nonreflecting outflow boundary condition for subsonic Navier-Stokes calculations, J. Comput. Phys. 36 (1980) 55-70.
[11] T. J. Poinsot and S. K. Lele, Boundary Conditions for Direct Simulations of
103
Compressible Viscous Flows, J. Comput. Phys. 101 (1992) 104-129.
[12] W. Polifke, C. Wall and P. Moin, Partially reflecting and non-reflecting boundary conditions for simulation of compressible viscous flow, J. Comput. Phys. 202 (2005) 710–736.
[13] W. S. Fu, C. G. Li, C. C. Tseng, An investigation of a dual-reflection phenomenon of a natural convection in a three dimensional horizontal channel without Boussinesq assumption, Int. J. Heat Mass Transfer 53 (2010)1575-1585.
[14] W. S. Fu, W. H. Wang, and S. H. Huang, An investigation of natural convection of three dimensional horizontal parallel plates from a steady to an unsteady situation by a CUDA computation platform, Int. J. Heat Mass Transfer 55 (2012) 4638-4650.
[15] C. Yoo, Y. Wang, A. Trouvé and H. Im, Characteristic boundary conditions for direct simulations of turbulent counterflow flams, Combustion Theory and Modeling 9 (4) (2005) 617-646.
[16] G. Lodato, P. Domingo and L. Vervisch, Three-dimensional boundary conditions for direct and large-eddy simulation of compressible viscous flows, J. Comput. Phys.
227 (2008) 5105-5143.
[17] J. P. Berenger, A perfectly matched layer for the absorption of electromagnetic waves, J. Comput. Phys. 114 (1994)185-200.
[18] F. Q. Hu, On absorbing boundary conditions of linearized Euler equations by a perfectly matched layer, J. Comput. Phys. 129 (1996)201-219.
[19] F. Q. Hu, On perfectly matched layer as an absorbing boundary condition, AIAA Paper (1996) 96-1664.
[20] S. Abarbanel and D. Gottlieb, A mathematical analysis of the PML method", J.
Comput. Phys. 134 (1997)357-363.
[21] J. S. Hesthaven, On the analysis and construction of perfectly matched layers for the linearized Euler equations, J. Comput. Phys.142 (1998)129-147.
104
[22] C. K. W. Tam, L. Auriault and F. Cambulli, Perfectly matched layer as an absorbing boundary condition for the linearized Euler equations in open and ducted domains, J. Comput. Phys. 144 (1998)213-234.
[23] F. Q. Hu, A stable, perfectly matched layer for linearized Euler equations in unsplit physical variables, J. Comput. Phys. 173 (2001)455 -480.
[24] M. Israeli and S. A. Orszag, Approximation of radiation boundary conditions, J.
Comput. Phys. 41 (1981)115 - 135.
[25] R. Kosloff and D. Kosloff, Absorbing boundary conditions for wave propagation problems, J. Comput. Phys. 63 (1986)363-376.
[26] T. Colonius, Lele, K. Sanjiva, Moin and Parviz, Boundary conditions for direct computation of aerodynamic sound generation, AIAA 31(9) (1993)1574-1582.
[27] S. Ta’asan, D. M. Nark, An Absorbing Buffer Zone Technique for Acoustic Wave Propagation, AIAA Aerospace Sciences Meeting and Exhibit (1995).
[28] B. Wasistho, B. J. Geurts and J. G. M. Kuerten, Simulation techniques for spatially evolving instabilities in compressible flow over a flat plate, Computers &
Fluids 26(7) (1997)713-739.
[29] J. B. Freund, Proposed Inflow/Outflow Boundary Condition for Direct Computation of Aerodynamic Sound, AIAA 35(4) (1997)740-742.
[30] W.S. Fu, C.G. Li, Y. Huang, The Application of CFD inComputing Jet Flow's Aeroacoustics, The 7th International Conference on Flow Dynamics (2010).
[31] T. Brandvik, G. Pullan, Acceleration of a 3D Euler solver using commodity graphics hardware, AIAA Aerospace Sciences Meeting and Exhibit (2008).
[32] A. Corrigan, F.F. Camelli, R. Lohner, J. Wallin, Running unstructured grid-based CFD solvers on modern graphics hardware, Int. J. Numer. Methods Fluids 66 (2010) 221-229.
[33] W.S. Fu, C.G. Li, Accelerate the CFD performance by using graphic hardware,
105
The 6th International Conference on Flow Dynamics (2009).
[34] W. S. Fu, W. H. Wang, Y. Huang and C. G. Li, An investigation of compressible forced convection in a three dimensional tapered chimney by CUDA computation platform, Int. J. Heat Mass Transfer 54 (2011)3420-3430.
[35] D. Jespersen, T. Pulliam, P. Bunung, Recent Enhancements to Overflow, AIAA, Aerospace Sciences Meeting and Exhibit, 35th, Reno, NV, 1997.
[36] I. Abalakin, A. Dervieux, and T. Kozubskaya, A vertex centered high order MUSCL scheme applying to linearized Euler acoustics, INRIA (2002) No4459.
[37] S. Yoon and S. Jameson, Lower-upper symmetric-Gauss-Seidel method for the Euler and Navier-Stokes equations, AIAA 26 (1988) 1025-1026.
[38] G. V. Candler and M. J. Wright, Data-Parallel Lower-Upper Relaxation Method for Reacting Flows, AIAA 32 (1994) 2380-2386.
[39] Nvidia. (n. d. ). CUDA C Programming Guide. Retrieved February 5, 2014, from http://docs.nvidia.com/cuda/cuda-c-programming-guide.
[40] O. Turgut and N. Onur, An experimental and three-dimensional numerical study of natural convection heat transfer between two horizontal parallel plates, Int.
Communication in Heat and Mass Transfer 34 (2007) 644-652.
[41] O. Manca and S. Nardini, Experimental investigation on natural convection in horizontal channels with the upper wall at uniform heat flux, Int. J. Heat Mass Transfer 50 (2007) 1075-1086.
[42] J.C.R. Hunt, A.A. Wray, P. Moin, Eddies, Stream and Convergence Zones in Turbulent Flows, Report CTR-S88, Center for Turbulence Research, 1988.