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1.
对13个不同翅片间距、翅片高度、横向管间距、纵向管间距的螺旋翅片管束换热器在不同雷诺数条件下的传热和阻力特性进行了试验研究,得出了翅片间距、翅片高度、横向管间距、纵向管间距及雷诺数与换热特性Nu和阻力特性Eu的准则关系式,并对准则关系式进行了分析.结果表明:随着横向管间距和翅片间距的增大,螺旋翅片管的传热得到强化,但随着纵向管间距和翅片高度的增加,螺旋翅片管的传热有所减弱;随着横向管间距、纵向管间距和翅片间距的增大,螺旋翅片管的阻力减少,但随着翅片高度的增加,螺旋翅片管的阻力增加.  相似文献   

2.
板翅式换热器翅片及隔板动态特性分析   总被引:1,自引:0,他引:1  
基于板翅式换热器翅片的非稳态导热方程,计算分析了翅片的动态特性,认为翅片的不稳定传热过程相对于换热器其它过程特征时间无限小,因此可以不考虑翅片的动态特性,从而简化了板翅式换热器动态模型,通过分析换热器动态过渡过程表明:隔板的热容对板翅式换热器的动态特性的影响是不容忽略的。  相似文献   

3.
为了解决百叶窗板翅式换热器的内部性能优化问题,通过对层流稳态下换热器燃气侧的典型流动换热单元进行建模及流动换热分析,得到了单元体内部速度、流线及温度的分布特性,并通过对换热系数、科尔本传热因子、进出口单位压降、范宁摩擦系数的比较,获得了不同燃气入口速度下翅片间距及翅片角度对换热器换热性能及流动阻力的影响。结果表明:在百叶窗翅片角度及其他尺寸参数不变时,当百叶窗间距为0. 7 mm时其换热性能最优,阻力随间距增大而减小;在翅片间距等参数不变而角度变化时,换热性能与阻力均随角度增大而增大,当百叶窗角度从15°增加至30°时,换热性能的增加幅度较为明显。  相似文献   

4.
利用SolidWorks三维绘图软件、HyperMesh网格划分工具以及Fluent数值计算软件研究了汽车换热器的翅片传热与阻力特性,分析了翅片高度、翅片节距对翅片传热与阻力特性的影响,得出了翅片传热因子和摩擦因子关于雷诺数以及翅片结构参数的计算关联式,对于实现换热器的高效设计,减少设计周期及成本,以及对汽车换热器的研究和行业的发展具有一定的参考意义。  相似文献   

5.
针对微型燃气轮机板翅式换热器结构参数与燃气轮机性能之间的耦合关系,建立了板翅式换热器多目标分析和优化模型。在此基础上,分析了2种设计条件(定燃烧室吸热量和定涡轮出功)下板翅式换热器关键参数对板翅式换热器和燃气轮机性能的影响。结果表明:影响燃烧室吸热量和涡轮出功的主要因素为换热器压损而并非换热器效能,2种设计条件下各参数的变化趋势一致(除燃烧室吸热量和涡轮出功外);在对翅片结构进行优化后,涡轮出功增大了6.8%,燃烧室吸热量减少了5.1%;相对于基本参数,优化后翅片厚度、翅片间距和波纹角减小,翅片高度增加,保证了板翅式换热器具有较小的压损;采用■耗散最小和采用熵产最小为优化目标时无明显区别。  相似文献   

6.
选取矩形截面平直翅片板翅式换热器的矩形单通道运用fluent软件进行数值模拟。首先对不同波高和波距的三组九种几何尺寸的翅片在同一工况下进行数值模拟,选出每组中传热和阻力综合性能最优者。然后对选出的三种翅片在不同工况下进行数值模拟,最终选出一种传热和阻力综合性能最优的。并对实物换热器进行试验研究,同时将试验结果和数值模拟结果进行对比分析,验证了数值模拟的正确性。  相似文献   

7.
为了获得管间距对开缝翅片管换热器传热与阻力特性的影响规律,对5种不同翅片管换热器进行了数值模拟研究,并进行了模化试验验证。结果表明:开缝翅片管束的传热和阻力特性与翅片侧气体的Re数有关,随着Re数增大,翅片侧Nu数增大,摩擦因子f逐渐减小;纵向间距S2对开缝翅片管换热器的综合流动传热性能的影响较大。数值模拟与试验结果偏差较小,采用数值模拟方法能够比较准确地分析开缝翅片管换热器的传热与阻力特性。  相似文献   

8.
《动力工程学报》2015,(11):893-900
基于板式换热器的研究成果,对板壳式换热器进行实验研究,利用等流速法求解传热准则关系式.通过控制冷流体、热流体流速相同,对1/1流程组合的板壳式换热器进行实验,并对比和分析实验数据.结果表明:利用板式换热器的经验值拟合得到的传热准则关系式在不同定性温度下并不相同;1/1流程组合板壳式换热器冷流体、热流体的传热准则关系式的参数均为定值,即系数为0.182 5,雷诺数指数为0.75,普朗特数指数为0.34;板壳式换热器的传热准则关系式与板程流程数无关,且与壳程1流程和2流程也无关,但与3流程和4流程则呈现出系数相关的结论,3流程和4流程的系数分别为1流程的0.82倍和0.68倍.  相似文献   

9.
多股流板翅式换热器温度交叉的数值分析   总被引:1,自引:1,他引:0       下载免费PDF全文
以平行多股流板翅式换热器为研究对象,给出了考虑翅片旁通作用的多股流板翅式换热器流体和翅片的能量方程。在改变多股流板翅式换热器各通道的流体参数、流动方式及换热器的结构参数等情况下,对能量方程进行数值求解,获得了各通道的流体温度分布情况及相邻通道的流体温度差,并分析了流体参数、流动方式和结构参数的变化对相邻通道流体温度交叉的影响。  相似文献   

10.
1.紧凑式换热器最近Frost&Sullivan公司作了一次市场调研,预期板框式、紧凑式换热器的增长率,在欧州和美国分别为22.9%和11.6%,而管壳式换热器分别为17.2和13.7%。紧凑式换热器单位体积的传热面积大,约高达700~1000m2/m3,比管壳式换热器要紧凑得多,典型的流道尺寸约为25mm,一些通用型式的紧凑式换热器有:板式、板翅式、螺旋板式和印刷电器式换热器。2.计算机化的流体动力学目前采用最多的设计软件是使用半经验方法,得出换热器中流动和传热的大致特征预测值,但并不精确和详尽。然而计算机和软件的进步用于经济地求解描…  相似文献   

11.
介绍了一次表面的发展及目前国内外研究的状况,采用单吹瞬变法对自行设计的3种CC(Cross Corrugated)型一次表面进行传热与阻力特性的试验研究.建立了数学模型,由数值解求得流体的出口温度与时间及传热单元数NTU间的函数关系.通过配比,获得了换热表面在测定工况下的NTU值.首次获得该3种CC表面的j和f的试验关联式.j因子和f因子均随Re的增加而逐渐下降,符合紧凑表面传热性能和阻力性能的一般规律.经误差分析,所提供的试验关联式的拟合误差不大于15%,具有足够的工程精度.关联式的使用条件是Re=120~800,换热面当量直径为1.2~1.4 mm,交错角45~75°.采用综合评价因子j/f对3种表面的性能进行了分析,结果表明,宽高比较大的型面具有较佳的综合性能.所得数据还与国内外其他学者的数值模拟结果进行了比较,试验数据与数值模拟的结果基本符合.  相似文献   

12.
Experimental studies were conducted to investigate the air-side heat transfer and pressure drop characteristics of a novel louvered fins and flat tube heat exchangers. A series of tests were conducted for 9 heat exchangers with different fin space and fin length, at a constant tube-side water flow rate of 2.8 m3/h. The air side thermal performance data were analyzed using the effectiveness-NTU method. Results were presented as plot of Colburn j factor and friction factor f against the Reynolds number in the range of 500–6500. The characteristics of the heat transfer and pressure drop of different fin space and fin length were analyzed and compared. In addition, the curves of the heat transfer coefficients vs. pumping power per unit heat transfer area were plotted. Finally, the area optimization factor was used to evaluate the thermal hydraulic performance of the louvered fins with differential geometries. The results showed that the j and f factors increase with the decrease of the fin space and fin length, and the fin space has more obvious effect on the thermal hydraulic characteristics of the novel louvered fins.  相似文献   

13.
本文利用CFD计算软件star ccm+,建立了管带式散热器空气侧的三维热固耦合模型,分析了不同空气流速和百叶窗结构参数对散热器流动和传热特性的影响,发现阻力损失主要集中在空气进入百叶窗的入口区域,百叶窗的前端传热效果较好,同时计算区域后半部分存在滞止区域;随着百叶窗倾角的增大,传热j因子先增后减,摩擦f因子一直增加,24°时传热j因子达到最大值;随着百叶窗厚度的增大,传热效果变差,摩擦f因子先增后减;百叶窗间距增加到一定程度,传热j因子和摩擦f因子增加缓慢,甚至减小。  相似文献   

14.
Three-dimensional CFD simulations are carried out to investigate heat transfer and fluid flow characteristics of a four-row plain fin-and-tube heat exchanger using the Commercial Computational Fluid Dynamics Code ANSYS CFX 12.0. Heat transfer and pressure drop characteristics of the heat exchanger are investigated for Reynolds numbers ranging from 400 to 2000. Fluid flow and heat transfer are simulated and results compared using both laminar and turbulent flow models (k-ω) with steady and incompressible fluid flow. Model validation is carried out by comparing the simulated case friction factor (f) and Colburn factor (j) with the experimental data of Wang et al. [1]. Reasonable agreement is found between the simulations and experimental data. In this study the effect of geometrical parameters such as fin pitch, longitudinal pitch and transverse pitch of tube spacing are studied. Results are presented in the form of friction factor (f) and Colburn factor (j). For both laminar and transitional flow conditions heat transfer and friction factor decrease with the increase of longitudinal and transverse pitches of tube spacing whereas they increase with fin pitches for both in-line and staggered configurations. Efficiency index increases with the increase of longitudinal and transverse pitches of tube spacing but decreases with increase of fin pitches. For a particular Reynolds number, the efficiency index is higher in in-line arrangement than the staggered case.  相似文献   

15.
百叶窗翅片作为换热器主要翅片形式之一,其结构对空气侧流动换热特性有着重要影响。本文总结了近年来国内外在百叶窗翅片结构对空气侧流动换热影响方面的研究,包括翅片间距、翅片高度、翅片厚度、翅片深度、百叶窗间距及开窗角度对空气侧换热系数、压降、流动效率、传热因子和摩擦因子的影响。研究表明:传热因子随开窗角度和翅片深度的增加而增大,随翅片间距的增加而减小;摩擦因子随开窗角度的增大而增大,随百叶窗间距的增大而减小;其中,开窗角度与翅片深度分别是影响空气侧流动和换热的最主要因素。最后,在百叶窗结构的基础上,提出了对翅片表面进行处理以及使用新型翅片结构等途径来进一步强化空气侧流动换热的建议。  相似文献   

16.
董军启  陈江平  袁庆丰  陈芝久 《动力工程》2006,26(6):871-874,903
风洞试验台上对8种不同结构参数的百叶窗翅片进行传热和流动阻力的性能试验。分析比较了翅片长度、翅片间距、翅片高度对其传热和阻力性能的影响,其中翅片长度和翅片间距对无量纲传热j因子和摩擦阻力f因子影响较大,翅片高度影响较小。同时采用3√j/f因子综合评价了8种翅片的强化传热效果。结果表明,翅片长度对强化传热影响最为显著。  相似文献   

17.
This study introduces the ability of Adaptive Neuro-Fuzzy Inference System (ANFIS) and genetic algorithm (GA) based correlations for estimating the hydrodynamics and heat transfer characteristics in coiled tubes. The experimental data related to the heat transfer and pressure drop in helically coiled tubes with deferent geometrical parameters (coil diameter and pitch) were used. In the experiments, hot water was passed in the coiled tubes, which were placed in a cold bath. Two ANFIS models were developed for predicting the Nusselt number (Nu) and friction factor (f) in the coiled tubes and the geometric parameters were employed as input data. Moreover, empirical correlations for estimating the Nu and f were developed by a phenomenological argument in the form of classical power–law correlations and their constants were found using the GA technique. The mean relative errors (MRE) of the developed ANFIS models for estimation of Nu and f are 6.24% and 3.54%, respectively. On the other hand, for empirical correlations, a MRE of 8.06% was found for prediction Nu while MRE of 5.03% was obtained for f. The results show that the ANFIS models can predict Nu and f with the higher accuracy than the developed correlations.  相似文献   

18.
对空气在锯齿型翅片内部流动和传热建立了三维数值计算模型,获得了五种不同流动角度下流体的温度场图、压力场图,摩擦因子,传热因子等重要数据,并通过这些图形、数据对流体流动特性和传热性能进行了比较,计算结果与文献所提供的实验数据进行对比,在整个计算范围内,传热因子j和摩擦因子f的平均偏差分别为6%和11%,所以运用CFD技术对研究不同流动角度下锯齿型翅片传热强化具有重要的指导意义。  相似文献   

19.
本文以两台波纹铝板空气一空气热交换器为例,对其传热和阻力特性进行了实验研究,得出了雷诺数在900~4000范围内,传热因子j和平均摩擦阻力系数f随雷诺数的变化规律,并分析了热交换器结构和不同强化传热元件对其换热和阻力特性的影响。  相似文献   

20.
An analogy was found between the frictional pressure drop and the heat transfer in liquid–solid circulating fluidized beds. This investigation is based on the predicting correlations for the particle holdup, the heat transfer coefficient, and the pressure drop, which were all developed by the authors. When the heat transfer coefficients were expressed in terms of the modified j‐factor, then a close mutual relationship was observed between the modified j‐factor and the friction factor of the pressure drop due to liquid and particle flow. A correlation to express this mutual relationship was derived, which consists of the density ratio of particle to liquid and the non‐dimensional riser diameter. The heat transfer coefficient predicted from the derived correlation agreed well with the experimental data by the authors, and with existing data. © 2009 Wiley Periodicals, Inc. Heat Trans Asian Res; Published online in Wiley InterScience ( www.interscience.wiley.com ). DOI 10.1002/htj.20246  相似文献   

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