In this paper, air side heat transfer and pressure drop characteristics of twelve three-row plate finandtube heat exchanger cores of four types of fin configurations have been experimentally investigated.The heat tran...In this paper, air side heat transfer and pressure drop characteristics of twelve three-row plate finandtube heat exchanger cores of four types of fin configurations have been experimentally investigated.The heat transfer and friction factor correlations for'the twelve cores are provided in a wide range ofReynolds number. It is found that in the range of Reynolds number tested, the Nusselt number of theslotted fin surface is the largest and that of the plain plate fin is the lowest while the Nusselt numbersof two types of wavy fins are somewhere in between.展开更多
利用粒子图像测速(PIV,particle i mage veloci metry)技术和红外热成像技术对增压空冷器空气侧的4排叉排圆弧型和X型开缝翅片的流动和传热特性进行了可视化试验研究。在试验的Reynolds数范围内,得到了阻力和换热特性曲线以及能反映流...利用粒子图像测速(PIV,particle i mage veloci metry)技术和红外热成像技术对增压空冷器空气侧的4排叉排圆弧型和X型开缝翅片的流动和传热特性进行了可视化试验研究。在试验的Reynolds数范围内,得到了阻力和换热特性曲线以及能反映流动和传热细节的流场和温度场。试验结果表明:X型开缝翅片的波动强度、流动阻力大于圆弧型开缝翅片,但前者的换热性能和场协同性优于后者。提出的新概念波动强度是表征翅片结构对流场扰动程度的物理量,波动强度越大,流场内的速度梯度、涡量强度越大,翅片结构对流场的扰动越大。可视化的试验结果为后续的数值模拟和翅片结构优化设计提供了可靠的试验依据。展开更多
文摘In this paper, air side heat transfer and pressure drop characteristics of twelve three-row plate finandtube heat exchanger cores of four types of fin configurations have been experimentally investigated.The heat transfer and friction factor correlations for'the twelve cores are provided in a wide range ofReynolds number. It is found that in the range of Reynolds number tested, the Nusselt number of theslotted fin surface is the largest and that of the plain plate fin is the lowest while the Nusselt numbersof two types of wavy fins are somewhere in between.
文摘利用粒子图像测速(PIV,particle i mage veloci metry)技术和红外热成像技术对增压空冷器空气侧的4排叉排圆弧型和X型开缝翅片的流动和传热特性进行了可视化试验研究。在试验的Reynolds数范围内,得到了阻力和换热特性曲线以及能反映流动和传热细节的流场和温度场。试验结果表明:X型开缝翅片的波动强度、流动阻力大于圆弧型开缝翅片,但前者的换热性能和场协同性优于后者。提出的新概念波动强度是表征翅片结构对流场扰动程度的物理量,波动强度越大,流场内的速度梯度、涡量强度越大,翅片结构对流场的扰动越大。可视化的试验结果为后续的数值模拟和翅片结构优化设计提供了可靠的试验依据。
