共查询到20条相似文献,搜索用时 78 毫秒
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实验研究了三角形硅微通道中的流动冷凝.通道中的冷凝流型沿程主要有珠状流、环状流、喷射流和弹状-泡状流等.在同一通道中,喷射流位置随着工质流量的增大而延后;在相同蒸气入口雷诺数下,喷射流位置则随着通道尺度的增大而延后.喷射流频率随着蒸气入口雷诺数和冷凝液韦伯数的增大而增大.较小水力直径的三角形通道中的流动冷凝不稳定性较高.冷凝通道的壁面温度呈沿程下降趋势.在同一通道中,流动冷凝的平均冷凝传热系数和平均努塞尔数,皆随着蒸气入口雷诺数的增大而增大,通道尺度的减小显著强化冷凝传热. 相似文献
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陶瓷微通道内的传热和压降特性 总被引:2,自引:0,他引:2
本文对一种新型陶瓷微通道换热器的传热与流动阻力特性进行了实验研究。实验工质分别为3M公司的HFE-7100和水。对于HFE7100流体,在传热面温度为40℃时热流密度可达10W/cm~2;对于水,传热面温度为35℃时热流密度可达约13W/cm~2。流动阻力特性实验结果表明,无论对于水还是HFE7100流体,在本实验范围内压降小于4.8kPa。 相似文献
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以工程上常用的66%的乙二醇水溶液作为工质,对几何特性相似而高宽比不同的4种纯铝矩形微通道内的流动特性进行了实验研究,得到了微通道冷板基础性的设计数据。实验测量了Reynolds数在50~500之间的流动阻力系数。实验结果表明:通道高度H与宽度W之比对微通道流阻特性有显著的影响;当Re数小于100时,在实验误差内,流动阻力系数的值近似等于经典理论计算值;随着Re数的增大和高宽比的变化,f的值远大于理论值,这可能是由微通道内部壁面粗糙度效应所导致的。 相似文献
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The present paper is devoted mainly to the half space problem for stationary Boltzmann-type equations. Using only conservation laws and the Boltzmann H-theorem we derive an inequality for unknown constant fluxes of mass, energy, and momentum. This inequality is expressed in terms of three parameters (pressure p, temperature T and the Mach number M) of the asymptotic Maxwellian at infinity. Geometrically the inequality describes a physical domain with positive entropy production in the 3-d space of the parameters. The domain appears to be qualitatively different for evaporation and condensation problems. We show that for given M, the curve p=p(M), T=T(M) of maximal entropy production practically coincides with the experimental evaporation curve obtained by Sone et al. on the basis of numerical solutions of BGK equation. Similar consideration for the condensation problem is also in qualitative agreement with known numerical results. 相似文献
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Forced convection heat transfer from a helically coiled heat exchanger embedded in a packed bed of spherical glass particles was investigated experimentally. With dry air at ambient pressure and temperature as a flowing fluid, the effect of particle size, helically coiled heat exchanger diameter, and position was studied for a wide range of Reynolds numbers. It was found that the particle diameter, the helically coiled heat exchanger diameter and position, and the air velocity are of great influence on the convective heat transfer between the helically coiled heat exchanger and air. Results indicated that the heat transfer coefficient increased with increasing the air velocity, increasing helically coiled heat exchanger diameter, and decreasing the particle size. The highest heat transfer coefficients were obtained with the packed-bed particle size of 16 mm and heat exchanger coil diameter of 9.525 mm (1/4 inch) at a Reynolds number range of 1,536 to 4,134 for all used coil positions in the conducted tests. A dimensionless correlation was proposed for Nusselt number as a function of Reynolds number, particle size, coil size, and coil position. 相似文献
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本文通过实验研究了CO2质量分数为11.39%~70.95%,壁面过冷度为5~25 K,总压力为5~15 kPa的CO2/H2O混合气体自然对流条件下在水平管外的凝结换热规律,结果表明CO2/H2O的凝结换热系数随CO2含量和壁面过冷度的增大而降低,但随总压力的增大而增大。根据实验结果建立了新关联式,将关联式应用到凝汽器的设计计算与分析,且对凝汽器进行了分离特性和经济性分析。 相似文献
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In this work, a double-layered microchannel heat exchanger is designed for investigation on gas-to-gas heat transfer. The micro-device contains 133 parallel microchannels machined into a polished polyether ether ketone plate for both the hot side and cold side. The microchannels are 200 μm high, 200 μm wide, and 39.8 mm long. The design of the micro-device allows tests with partition foils in different materials and of flexible thickness. A test rig is developed with the integration of customized pressure and temperature sensors for in situ measurements. Experimental tests on the counter-flow micro heat exchanger have been carried out for five different partition foils and various mass flow rates. The experimental results, in terms of pressure drop, heat transfer coefficients, and heat exchanger effectiveness are discussed and compared with the predictions of the classic theory for conventionally sized heat exchangers. 相似文献
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大量采用宇航级元器件进行航天器研制的模式,由于其“成本高、研制周期长、元器件性能不足”等缺点,已经难以满足微纳卫星“周期短、成本低、集成度高”的要求。因此提出了在微纳卫星上使用COTS(Commercial off-the-shelf)器件的方法;针对微纳卫星的特点,首先分析了微纳卫星对COTS器件的需要和风险,提出了COTS器件微纳卫星应用的选用原则、选用依据;在此基础上经过分析,提出了COTS元器件微纳卫星应用流程,有针对性提出了COTS器件应用的器件级和板级筛选方法,并开展了COTS器件的微纳卫星抗单粒子效应加固设计,进一步提高COTS器件应用的可靠性。通过在轨应用验证,结果表明,通过该方法选用筛选的COTS器件,在进行有效加固后可以满足微纳卫星在轨稳定运行的要求,同时为微纳卫星降低成本缩短研制周期提供了保障。该方法对COTS器件在微纳卫星中的应用提供了一般性指导意义。 相似文献
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Fengxun Hai 《中国物理 B》2022,31(6):64401-064401
While the influence of liquid qualities, surface morphology, and operating circumstances on critical heat flux (CHF) in pool boiling has been extensively studied, the effect of the heater substrate has not. Based on the force balance analysis, a theoretical model has been developed to accurately predict the CHF in pool boiling on a heater substrate. An analytical expression for the CHF of a heater substrate is obtained in terms of the surface thermophysical property. It is indicated that the ratio of thermal conductivity (k) to the product of density (ρ) and specific heat (cp) is an essential substrate property that influences the CHF. By modifying the well-known force-balance-based CHF model (Kandlikar model), the thermal characteristics of the substrate are taken into consideration. The bias of predicted CHF values are within 5% compared with the experimental results. 相似文献