首页> 外文会议>2007 Asian symposium on computational heat transfer and fluid flow >EXPERIMENTAL AND NUMERICAL INVESTIGATION OF THERMAL -HYDRAULIC PERFORMANCE IN WAVY FIN-AND-FLAT TUBE HEAT EXCHANGERS
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EXPERIMENTAL AND NUMERICAL INVESTIGATION OF THERMAL -HYDRAULIC PERFORMANCE IN WAVY FIN-AND-FLAT TUBE HEAT EXCHANGERS

机译:波浪形翅片管换热器热工水力性能的实验和数值研究

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To more deeply understand the enhanced heat transfer mechanism and optimization design for wavy fin and flat tube heat exchangers, three-dimensional numerical simulations and experimental investigation of air flow and heat transfer characteristics are presented in this study. The numerical simulation results compared with the wind tunnel test data, the results show that the numerical simulation results are in good agreement with the test. The experimental results show that the flow transition from laminar to turbulent occurs at earlier Reynolds number around 1000. In the range of Re=1000-5500, the standard k-ε mode (SST) is more suitable to predict the air flow and heat transfer of wavy fin. The waviness amplitude has the distinct effect on the heat transfer and pressure drop of wavy fin, while the wavy fin profile (Triangular, Sinusoidal and Triangular round corner) has little effect on the heat transfer performance. In additional, the enhanced heat transfer mechanism of wavy fin is explained in view of field synergy principle. Reduction the synergy angle between velocity and temperature gradient will lead to increase the heat transfer coefficients of wavy fin.
机译:为了更深入地了解波纹翅片和扁平管式换热器的强化传热机理和优化设计,本研究提出了三维数值模拟以及气流和传热特性的实验研究。数值模拟结果与风洞试验数据进行了比较,结果表明数值模拟结果与试验结果吻合良好。实验结果表明,从层流到湍流的流变发生在早于大约1000的雷诺数处。在Re = 1000-5500的范围内,标准k-ε模式(SST)更适合于预测空气流动和传热波浪鳍。波纹幅度对波状翅片的传热和压降有明显的影响,而波状翅片轮廓(三角形,正弦形和三角形圆角)对传热性能的影响很小。另外,根据场协同原理解释了波浪状翅片的增强的传热机理。减小速度和温度梯度之间的协同角将导致波浪状翅片的传热系数增加。

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