结霜等截面环肋传热特性

通过适当假设,推导出了结霜等截面环肋传热的数学模型,然后得到其传热热问题的修正解,同时给出其相应的热流量计算公式。与一般简化的肋传热计算公式相比,该解提高了计算精度,并且表达形式简单,可以很方便的应用于工程实践;对结霜肋片的设计有一定的理论指导作用,并可以推广到其他类似的传热等问题中。     

结霜等截面直肋导热修正解

通过适当假设,推导出了结霜等截面直肋导热的数学模型,然后得到其导热问题的修正解,同时给出其相应的热流量计算公式。与原先的肋导热计算公式相比,该解提高了计算精度,并且表达形式简单,可以很方便的应用于工程实践。对结霜肋片的设计有一定的理论指导作用,而且其求解方法可以推广到类似的问题中。     

低温工况下冷风机结霜性能研究

文中以冷风机为研究对象,首先对低温工况下冷风机的结霜性能进行理论分析,并建立数学模型;其次通过实验,分析了结霜对翅片管效率、空气侧平均换热系数和空气侧压降的影响。结果证明:数值计算的结果和实验测试结果基本吻合,从而证明了数学模型的正确性与可靠性。     

换热器低温结霜工况性能实验研究

利用搭建的换热器低温结霜工况性能实验台,测试了在不同的入口空气温度、湿度、流速等环境参数下,翅片管蒸发器低温结霜工况的结霜量、制冷量、进出口空气侧压降和能量传递系数的变化以及结霜量、制冷量、空气侧压降和能量传递系数等随霜层增长的变化规律,分析了环境参数对翅片管蒸发器性能的影响,为低温条件下换热器动态结霜性能研究提供了更多的实验参考和计算依据。     

不同壁面结构与传热情形下低温壁面结霜特性

壁面结霜致使低温换热设备传热性能下降,甚而产生设备安全和生产安全问题。通过实验研究了涂覆疏水涂料壁面结构的结霜特性,不同倾斜角度壁面的水滴凝结与滑落特性,以及添置了太阳能吸热膜的表面传热特性。结果表明:涂有疏水材料的壁面较普通壁面初始结霜时间能延迟约10分钟;一定的壁面倾斜角度通过影响水滴的滚动角,促进凝结的水滴滑落,可阻碍霜层生长;当换热壁面利用太阳能吸热膜对低温壁面进行补热时,吸热量为5.27J/cm2,为普通壁面的1.44倍。这些改进措施可以减少冷壁面结霜量,有助于提升低温设备传热效果。     

不同壁面结构与传热情形下低温壁面结霜特性北大核心

壁面结霜致使低温换热设备传热性能下降,甚而产生设备安全和生产安全问题。通过实验研究了涂覆疏水涂料壁面结构的结霜特性,不同倾斜角度壁面的水滴凝结与滑落特性,以及添置了太阳能吸热膜的表面传热特性。结果表明:涂有疏水材料的壁面较普通壁面初始结霜时间能延迟约10分钟;一定的壁面倾斜角度通过影响水滴的滚动角,促进凝结的水滴滑落,可阻碍霜层生长;当换热壁面利用太阳能吸热膜对低温壁面进行补热时,吸热量为5.27J/cm2,为普通壁面的1.44倍。这些改进措施可以减少冷壁面结霜量,有助于提升低温设备传热效果。     

换热器低温结霜工况性能试验系统的研制

为了对换热器在低温结霜工况下的动态运行特性进行研究,设计搭建了换热器结霜工况性能实验台,安装了各参数测量仪表和传感器。实验台由制冷循环和模拟低温工况的风道循环两部分组成,并采用C#编程技术,基于.NET开发了集环境模拟、数据采集、显示和数据处理、实时曲线和视频显示功能于一体的远程测控系统,该试验系统的研制为低温结霜工况下换热器运行特性研究提供了更多的实验参考和计算依据。     

结霜工况下的冷风机传热性能试验研究

文中对冷风机在结霜工况下的传热性能进行了试验研究 ,简述了结霜工况下传热系数测试的原理、方法和主要过程。根据实验结果对影响冷风机传热性能的主要因素进行了分析 ,并得出了一些有益的结论     

竖直低温星形翅片管表面结霜及传热传质理论模型

文中采用维元法建立了竖直星形翅片管表面的非稳态结霜及传热传质模型,重点考虑了霜层表面存在的对流、凝华以及辐射三种传热机理。理论模型的计算结果表明,霜层的生长速度以及霜层表面的温度升高都是一个逐渐变缓的过程。在这个过程中,三种机理的传热分量也随之变化。同时,随着霜层厚度的增加,翅片管整体传热效率降低,管内过冷区和饱和区的长度都被拉长。     

低温工况下结霜对翅片管蒸发器性能影响的实验研究

翅片管蒸发器的结霜将增加空气压降 ,增大传热热阻 ,从而直接影响到蒸发器的效率及空气侧平均换热系数。文中就低温工况下结霜对蒸发器性能的影响进行了测试研究 ,为翅片管蒸发器的设计应用提供了重要依据     

Heat Transfer and Fluid Flow Characteristics of Microchannel with Oval-Shaped Micro Pin Fins

A novel microchannel heat sink with oval-shaped micro pin fins (MOPF) is proposed and the characteristics of fluid flow and heat transfer are studied numerically for Reynolds number (Re) ranging from 157 to 668. In order to study the influence of geometry on flow and heat transfer characteristics, three non-dimensional variables are defined, such as the fin axial length ratio (α), width ratio (β), and height ratio (γ). The thermal enhancement factor (η) is adopted as an evaluation criterion to evaluate the best comprehensive thermal-hydraulic performance of MOPF. Results indicate that the oval-shaped pin fins in the microchannel can effectively prevent the rise of heat surface temperature along the flow direction, which improves the temperature distribution uniformity. In addition, results show that for the studied Reynolds number range and microchannel geometries in this paper, the thermal enhancement factor η increases firstly and then decreases with the increase of α and β. In addition, except for Re = 157, η decreases first and then increases with the increase of the fin height ratio γ. The thermal enhancement factor for MOPF with α = 4, β = 0.3, and γ = 0.5 achieves 1.56 at Re = 668. The results can provide a theoretical basis for the design of a microchannel heat exchanger.     

低温预冷换热规律及表面改性影响研究

调研了低温管路预冷及两相换热的研究现状,阐述了低温预冷瞬态换热特性;介绍了金属表面改性对预冷规律的影响,仿真了低导热涂层管的预冷换热规律.研究发现:液氮预冷主要由膜态沸腾支配,且预冷耗时较长;液氢预冷未见膜态沸腾,预冷耗时更短.促进膜态沸腾向过渡沸腾的更早转化有利于预冷加速,且转化温度迁移可通过内壁表面结构改性实现,可...     

梭形百叶窗结构内传热强化数值分析

提出一种新型百叶窗结构—梭形百叶窗,它与一般的矩形百叶窗结构相比,流道从翅片中间截面到管连接处逐渐变宽,有较多流体冲刷管壁表面,增加管壁附近流体温度梯度,从而使传热增强。同时降低了流体流动阻力。具有较好的流动和传热性能。应用FLUENT软件对两种百叶窗结构下空气的流场、温度场和压力场进行了CFD研究,分析不同Re数对换热和流动性能的影响。     

Local Heat Transfer Distribution in a Rectangular Pin Channel With and Without Vortex Generators

Short pin fins are used to enhance heat transfer rates by increasing the level of turbulence in the trailing edge of gas turbine blades. Experiments are conducted to investigate the local Nusselt number distributions in a staggered pin-fin array using the infrared thermal imaging technique. The pin fins are arranged in a rectangular channel with an aspect ratio of 9. The pins have streamwise pitch-to-diameter (X_S/D) and spanwise pitch-to-diameter (X_T/D) ratios of 2 with a pin height-to-diameter (H/D) ratio of 2. Ejection holes of 5-mm diameter with a pitch of 12.7 mm are used to study the effects of lateral ejection. Both one-wall and two-wall heating situations are studied for straight-flow and lateral-ejection cases. It is found that the local Nusselt numbers are highest below the horseshoe vortices just upstream of the individual pin fins. For the straight-flow case, the Nusselt numbers for the two-wall heating case are observed to be 15–20% higher than those of the one-wall heating case. Lateral ejection causes a decrease of about 1–10% for the one-wall heating case, while there is an increase of about 10% for the two-wall heating case. Experiments are also carried out with vortex generators between individual pin fins. Vortex generators cause an increase in heat transfer by about 50% compared to the straight-flow cases.     

Experimental Investigation Of Spray Cooling Heat Transfer On Straight Fin Surface Under Acceleration Conditions

A spray cooling heat transfer experiment on straight fin surface under acceleration conditions was conducted to investigate the effects of acceleration, flow rate, and nozzle height. The results show that the acceleration can improve the heat transfer performance in a limited way. In addition, whether in the acceleration or stationary condition, the flow rate as well as the nozzle height has the same impact on the spray cooling performance. It is also observed that the surface temperature can influence the effect of flow rate on spray cooling performance, and the cooling performance becomes worse with the increase of nozzle height.     

伴随水力空化现象的对流换热数值研究

以水为介质,建立了液体流动的混合物多相流模型及空化模型,运用CFD方法对水平圆管内伴随有水力空化现象的受迫对流换热过程进行了数值研究,详细分析了管道入口压力、入口温度和限流孔与管道直径比等因素对水力空化及对流换热过程的影响规律。数值模拟结果表明,空化现象出现在圆管喉部(限流孔)壁面附近区域;与相同流量下无空化时的传热相比,在发生空化现象的区域,传热壁面被蒸汽所覆盖导致传热急剧恶化,而在远离空化发生区域的下游位置,由于空化的扰流作用使得加热壁面与流体之间的传热得到明显改善。     

Heat Transfer in Oscillating Circular Pipes

An experimental investigation was made to study heat transfer in a pipe which is oscillated about an axis that is parallel to, but offset from, the pipe axis. Air was used as working fluid. The experimental setup was designed so as to provide oscillating motion of a test pipe. The measurement systems were installed on the oscillating section. For both steady and oscillating flows, the bulk air temperature and wall temperature, pressure drop, and frequency were measured. The parameters for this study were chosen as Reynolds number from 5,000 to 20,000 and oscillating frequencies from 10 to 20 Hz. The variations of Nusselt number versus these parameters were determined and presented graphically. Heat transfer enhancement of 42% was achieved at constant pumping power for oscillatory flow.     

不同翅片单元外颗粒流换热特性的数值研究

由于成本低,运行稳定,重力驱动移动床在高温固体散料余热回收领域应用潜力较大.然而,相关强化传热技术目前仍待完善.本文基于离散单元法,对颗粒流外掠翅片单元的流动换热特性进行了数值研究.研究表明:通过翅片增加换热面,可以显著提高传热量,但不同翅片单元外颗粒流传热特性不同.颗粒流与不同表面的换热,由颗粒更新、颗粒接触、颗粒竞...     

Study on Heat Transfer Performance of Skin Heat Exchanger

Cooling technology is facing new challenges with the increase of electronic equipment power onboard aircraft. The traditional heat sink based on high-altitude bleed air does not satisfy this increase of cooling demands. In this article, an air/air-type skin heat exchanger is studied for cooling aircraft electronic equipment. It uses outside high-altitude cold air rather than bleed air as a heat sink. This cooling technology can effectively remove the heat load of high-power electronic devices without greatly increasing aircraft performance penalty. To assess its high-altitude heat transfer performance, an experimental prototype was designed and made. Some experiments were conducted on a ground experimental test. The heat transfer criteria formulas were obtained for both the side air in the skin heat exchanger and its convective heat transfer coefficients. Based on these experimental analyses, the heat transfer performances of the skin heat exchanger in a high-altitude cruise condition are deduced when it is assumed to be installed at an unfavorable position and a favorable position, separately. This work tries to provide a technical support for its future onboard application.