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A numerical analysis of power efficiency of wind rotor systems in a parallel matrix 并联矩阵中风力转子系统功率效率的数值分析
IF 1.5 Q2 Mathematics Pub Date : 2012-09-26 DOI: 10.1615/COMPUTTHERMALSCIEN.2012004748
Jia Feng, C. Tseng, Chiun-Hsun Chen
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引用次数: 2
NUMERICAL STUDY OF UNSTEADY AIRFLOW PHENOMENA IN A VENTILATED ROOM 通风室内非定常气流现象的数值研究
IF 1.5 Q2 Mathematics Pub Date : 2012-07-03 DOI: 10.1615/COMPUTTHERMALSCIEN.2012005093
K. Horikiri, Yufeng Yao, J. Yao
Numerical simulation of airflow in an indoor environment has been carried out for forced, natural, and mixed convection modes, respectively, by using the computational fluid dynamics (CFD) approach of solving the Reynolds-averaged Navier−Stokes equations. Three empty model rooms in two-dimensional configuration were studied first; focusing on the effects of grid refinement, mesh topology, and turbulence model. It was found that structured mesh results were in better agreement with available experimental measurements for all three convection scenarios, while the renormalized group (RNG) к − e turbulence model produced better results for both forced and mixed convections and the shear stress transport (SST) turbulence model for the natural convection prediction. Further studies of air velocity and temperature distributions in a three-dimensional cubic model room with and without an obstacle have shown reasonably good agreement with available test data at the measuring points. CFD results exhibited some unsteady flow phenomena that have not yet been observed or reported in previous experimental studies for the same problem. After analyzing the time history of velocity and temperature data using fast Fourier transformation (FFT), it was found that both air velocity and temperature field oscillated at low frequencies up to 0.4 Hz and the most significant velocity oscillations occurred at a vertical height of an ankle level (0.1 m) from the floor, where temperature oscillation was insignificant. The reasons for this flow unsteadiness were possibly a higher Grashof number, estimated at 0.5 × 106 based inflow conditions, and thus strong buoyancy driven effects caused the oscillations in the flow field. The appearance of an obstacle in the room induced flow separation at its sharp edges and this would further enhance the oscillations due to the unsteady nature of detached shear-layer flow.
利用计算流体动力学(CFD)方法求解reynolds -average Navier - Stokes方程,分别对室内环境中的强制对流、自然对流和混合对流模式进行了数值模拟。首先研究了三个二维构型的空样板房;重点研究网格细化、网格拓扑和湍流模型的影响。结果表明,在三种对流模式下,结构化网格计算结果与现有的实验测量结果吻合较好,而重整化群(RNG)湍流模型对强迫对流和混合对流的预测结果较好,剪切应力输运(SST)湍流模型对自然对流的预测结果较好。在有障碍物和没有障碍物的三维立方模型室内进行的进一步研究表明,风速和温度分布与测点的现有测试数据相当吻合。CFD结果显示了一些非定常流动现象,这些现象在以前的实验研究中没有观察到或报道过。在使用快速傅里叶变换(FFT)分析速度和温度数据的时间历史后,发现空气速度和温度场都在0.4 Hz的低频振荡,最显著的速度振荡发生在距离地板脚踝水平(0.1 m)的垂直高度,温度振荡不明显。这种流动不稳定的原因可能是较高的Grashof数,根据入流条件估计为0.5 × 106,因此强烈的浮力驱动效应导致了流场的振荡。室内障碍物的出现在其尖锐的边缘处引起了流动分离,这将进一步增强由于分离剪切层流动的非定常性而引起的振荡。
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引用次数: 13
A LATTICE MONTE CARLO ANALYSIS ON CHEMICAL REACTION WITH MOVING BOUNDARY 移动边界化学反应的晶格蒙特卡罗分析
IF 1.5 Q2 Mathematics Pub Date : 2012-06-20 DOI: 10.1615/COMPUTTHERMALSCIEN.2012003941
T. Fiedler, I. Belova, A. Öchsner, G. Murch
The current paper aims to simulate combined mass diffusion and chemical reaction. Two solid reactants are brought into contact and the product is formed at the interface. Chemical reaction is assumed to occur instantaneously, thus the reaction rate is limited only by the interdiffusion of the two solid constituents. First, parametric studies for a range of constant diffusivities are performed and simple relations for the growth of the product phase are obtained. It is found that the thickness of the product layer increases proportionally to the square root of the product of diffusivity and time. In the second part of the analyses the formation of NiAl by interdiffusion of nickel and aluminum is simulated. This self-propagating exothermic reaction is of great interest for joining temperature-sensitive components. Within the limits of these calculations, the concentration dependence of the diffusion coefficients of nickel and aluminum is considered in order to improve the accuracy of the simulation.
本文的目的是模拟质量扩散和化学反应的结合。两个固体反应物接触,产物在界面处形成。假定化学反应是瞬间发生的,因此反应速率仅受两种固体组分的相互扩散的限制。首先,对恒定扩散系数范围进行了参数化研究,得到了产物相生长的简单关系。结果表明,积层厚度与扩散系数与时间乘积的平方根成正比。第二部分模拟了镍与铝相互扩散形成NiAl的过程。这种自传播的放热反应对于连接温度敏感的组分很有意义。在这些计算的范围内,考虑了镍和铝扩散系数的浓度依赖性,以提高模拟的准确性。
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引用次数: 0
ZONAL RANS-LES MODELING FOR TURBINES IN AEROENGINES 航空发动机涡轮的纬向转捩建模
IF 1.5 Q2 Mathematics Pub Date : 2012-03-18 DOI: 10.1615/COMPUTTHERMALSCIEN.2012006402
P. Tucker, R. Jefferson-Loveday, J. Tyacke, V. N. Rao
The cost of large-eddy simulation (LES) modeling in various zones of gas turbine aeroengines is outlined. This high cost clearly demonstrates the need to perform hybrid Reynolds-averaged Navier-Stokes-LES (RANS-LES) over the majority of engine zones because the Reynolds number is too high for pure LES. The RANS layer is used to cover over the fine streaks found in the inner part of the boundary layer. The hybrid strategy is applied to various engine zones, which is shown to typically give much greater predictive accuracy than pure RANS simulations. However, the cost estimates show that the RANS layer should be disposed within the low-pressure turbine zone. Also, the nature of the flow physics in this zone makes LES most sensible. © 2012 by Begell House, Inc.
概述了燃气涡轮航空发动机各区域大涡模拟建模的成本。如此高的成本清楚地表明,在大多数发动机区域需要执行混合雷诺-平均纳维-斯托克斯-LES (ranss -LES),因为纯LES的雷诺数太高。RANS层用于覆盖在边界层内部发现的细条纹。混合策略应用于各种发动机区域,其预测精度通常比纯RANS模拟高得多。然而,成本估算表明,RANS层应布置在低压涡轮区。此外,该区域的流动物理性质使LES最合理。©2012 by Begell House, Inc。
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引用次数: 0
NUMERICAL SIMULATION FOR A FLOW AROUND BODY EJECTION USING AN AXISYMMETRIC UNSTRUCTURED MOVING GRID METHOD 用轴对称非结构移动网格法模拟绕体弹射流动
IF 1.5 Q2 Mathematics Pub Date : 2012-01-01 DOI: 10.1615/COMPUTTHERMALSCIEN.2012004715
M. Yamakawa, Daiki Takekawa, K. Matsuno, S. Asao
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引用次数: 8
BUBBLE DYNAMICS DURING POOL BOILING UNDER MICROGRAVITY CONDITIONS 微重力条件下池沸腾过程中的气泡动力学
IF 1.5 Q2 Mathematics Pub Date : 2012-01-01 DOI: 10.1615/COMPUTTHERMALSCIEN.2012006423
Dean Vijay K. Dhir, G. Warrier, Eduardo Aktinol
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引用次数: 3
NUMERICAL STUDY OF THE EFFECT OF HEAT LOSS ON TRIPLE FLAME PROPAGATION IN A POROUS WALLS CHANNEL 热损失对多孔壁面通道内三重火焰传播影响的数值研究
IF 1.5 Q2 Mathematics Pub Date : 2012-01-01 DOI: 10.1615/COMPUTTHERMALSCIEN.2012005345
F. Al-Malki
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引用次数: 6
PREFACE: ASIAN SYMPOSIUM ON COMPUTATIONAL HEAT TRANSFER AND FLUID FLOW-2011 (ASCHT-11) 前言:亚洲计算传热与流体流动研讨会-2011 (ascht-11)
IF 1.5 Q2 Mathematics Pub Date : 2012-01-01 DOI: 10.1615/COMPUTTHERMALSCIEN.2012005792
K. Suga, M. Shibahara
This special section consists of selected papers from the third Asian Symposium on Computational Heat Transfer and Fluid Flow (ASCHT-11) chaired by Prof. Hiroshi Kawamura of Tokyo University of Science, Suwa, held from 22 to 26 September, 2011 in Kyoto, Japan. As the two preceding symposia in Xi’an, China (2007) and Jeju, Korea (2009), the ASCHT-11 successfully attracted 169 delegates from a wide variety of countries: China, India, Iraq, Japan, Korea, Russia, Taiwan and UK (in alphabetical order). The ASCHT-11 was mainly operated by Heat Transfer Society of Japan, as one of her 50th anniversary events, and was held in cooperation with the International
本专题包括2011年9月22日至26日在日本京都举行的第三届计算传热和流体流动亚洲研讨会(ASCHT-11)的论文选集,该研讨会由东京科学大学的Hiroshi Kawamura教授主持。与前两次在中国西安(2007年)和韩国济州岛(2009年)举行的研讨会一样,ASCHT-11成功吸引了来自不同国家的169名代表:中国、印度、伊拉克、日本、韩国、俄罗斯、台湾和英国(按字母顺序)。ASCHT-11主要由日本传热学会运营,作为其50周年纪念活动之一,与国际合作举办
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引用次数: 0
COMPUTATIONAL AND EXPERIMENTAL INVESTIGATION ON THERMAL INSULATION CAPABILITIES OF RICE-HUSK FILLED EPOXY COMPOSITES 稻壳填充环氧复合材料保温性能的计算与实验研究
IF 1.5 Q2 Mathematics Pub Date : 2012-01-01 DOI: 10.1615/COMPUTTHERMALSCIEN.2012004213
A. Rout, A. Satapathy
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引用次数: 0
A robust Monte Carlo based ray-tracing approach for the calculation of view factors in arbitrary three-dimensional geometries 一种鲁棒的基于蒙特卡罗的光线追踪方法,用于计算任意三维几何中的视图因子
IF 1.5 Q2 Mathematics Pub Date : 2012-01-01 DOI: 10.1615/COMPUTTHERMALSCIEN.2012006084
T. Walker, S. Xue, G. Barton
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引用次数: 4
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