共查询到19条相似文献,搜索用时 109 毫秒
1.
2.
3.
随着高效预冷器在航天航空领域发挥越来越重要的作用,紧凑高效换热器的研究成为了人们关注的热点。本文基于紧凑微通道换热器的几何特征,针对矩形截面平行流道换热器内超临界压力低温流体(氢和氦)在大温差条件下的流动换热现象进行数值模拟研究。通道截面边长小于1 mm,热流体氦和冷流体氢的进出口温差均大于600 K。通道内流体换热系数在顺流和逆流条件下有不同的变化趋势,并出现峰值。换热量随着通道宽度的增大而增大,流动压降随着通道宽度的增大而减小。冷热流体逆流时换热量大,压降较小,但对换热器材料要求较高。 相似文献
4.
随着高效预冷器在航天航空领域发挥越来越重要的作用,紧凑高效换热器的研究成为了人们关注的热点。本文基于紧凑微通道换热器的几何特征,针对矩形截面平行流道换热器内超临界压力低温流体(氢和氦)在大温差条件下的流动换热现象进行数值模拟研究。通道截面边长小于1 mm,热流体氦和冷流体氢的进出口温差均大于600 K。通道内流体换热系数在顺流和逆流条件下有不同的变化趋势,并出现峰值。换热量随着通道宽度的增大而增大,流动压降随着通道宽度的增大而减小。冷热流体逆流时换热量大,压降较小,但对换热器材料要求较高。 相似文献
5.
6.
以CO_2为工质,对空气源热泵热水器矩形螺旋套管气体冷却器的换热特性进行实验研究,搭建了空气源热泵热水器实验台,测试分析冷却水流量的变化对冷却水进出口温差、CO_2进出口压力与温度、CO_2质量流量、气体冷却器总换热量、总传热系数及热泵系统COP等参数的影响,探究其对气体冷却器换热性能的变化规律。结果表明:随着冷却水流量的增加,冷却水进出口温差、CO_2进出口压力和温度均呈下降趋势,CO_2质量流量则呈上升趋势;气体冷却器的总换热量增加49.70%,总传热系数增加57.55%,COP增加73.41%,增幅较大;而气体冷却器换热效能系数仅增加1.77%,变化趋势不明显。 相似文献
7.
8.
采用两相流的流动换热理论,建立二维几何模型,运用FLUENT对稳定入口流速下注入气体的铅铋流动段作了模拟。模拟研究注入气体的体积份额或速度改变对压力和铅铋与注入气体之间换热与影响,得到了不同条件下的温度与压力分布。分析结果发现,体积份额减小,铅铋流体的径向温度分布更加均匀,中心温度更低;随着体积份额的减小,铅铋的总压呈现出一种下降的趋势。注入气体速度不同对铅铋整体的换热影响不大;中心处的动压有较大增加,总压改变甚微。 相似文献
9.
为研究粗糙表面对纳尺度流体流动和传热及其流固界面速度滑移与温度阶跃的影响,本文建立了粗糙纳通道内流体流动和传热耦合过程的分子动力学模型,模拟研究了粗糙通道内流体的微观结构、速度和温度分布、速度滑移和温度阶跃并与光滑通道进行了比较,并分析了固液相互作用强度和壁面刚度对界面处速度滑移和温度阶跃的影响规律. 研究结果表明,在外力作用下,纳通道主流区域的速度分布呈抛物线分布,由于流体流动导致的黏性耗散使得纳通道内的温度分布呈四次方分布. 并且,在固体壁面处存在速度滑移与温度阶跃. 表面粗糙度的存在使得流体剪切流动产生了额外的黏性耗散,使得粗糙纳通道内的流体速度水平小于光滑通道,温度水平高于光滑通道,并且粗糙表面的速度滑移与温度阶跃均小于光滑通道. 另外,固液相互作用强度的增大和壁面刚度的减小均可导致界面处速度滑移和温度阶跃程度降低.
关键词:
速度滑移
温度阶跃
流固界面
粗糙度 相似文献
10.
11.
12.
T. V. Bazhenova S. V. Golovastov V. V. Golub I. N. Laskin N. V. Semin 《Russian Journal of Physical Chemistry B, Focus on Physics》2009,3(6):917-922
The results of a numerical study of the pulsed outflow of hydrogen into an air-filled channel are presented. The adjustable parameters were the initial pressure of hydrogen in the reservoir and the distance from the diaphragm to the ignition point. The pressure, temperature, and water vapor mass fraction profiles along the channel wall at various moments of time were calculated. The autoignition parameters were calculated with account of turbulence, boundary layer formation, heat transfer, and diaphragm opening time. It was demonstrated that the boundary layer effect promotes hydrogen autoignition. The dependence of the distance from the diaphragm to the autoignition point was calculated as a function of the pressure in the reservoir with hydrogen. The simulation results were found to be in close agreement with the available experimental data. 相似文献
13.
The process of vapor transfer in conditions of linear change in temperature along the channel is considered. The excess pressure of the vapor-gas mixture above the liquid meniscus is calculated as a function of the capillary radius and temperature. Expressions are found for the vapor flux and time of evaporation. It is shown that these expressions are in good agreement with experimental data.Translated from Izvestiya Vysshikh Uchebnykh Zavedenii, Fizika, No. 5, pp. 65–70, May, 1984. 相似文献
14.
用T-Jump/FTIR在线联用分析技术,研究了GAP/AP混合体系在模拟燃烧条件下快速加热高温高压的热裂解。结果表明,GAP/AP混合体系的主要热裂解气相产物的组成发生了变化,说明组分之间存在相互作用。压力对GAP/AP混合体系气相产物有明显的影响,表明混合体系组分GAP和AP之间的相互作用是通过AP分解气相产物进行的,混合体系不但存在气相之间的反应,也存在气相/凝聚相反应。而温度并没有影响AP对GAP的作用。用T-Jump/FTIR在线分析技术能够实现模拟燃烧条件下含能材料实时气体产物分析,为从微观反应的角度探索含能材料的快速高压热裂解及其组分之间的相互作用提供一条技术途径。 相似文献
15.
Marco Schultze John Mantzaras Rolf Bombach Konstantinos Boulouchos 《Proceedings of the Combustion Institute》2013,34(2):2269-2277
The hetero-/homogeneous combustion of hydrogen/air mixtures over platinum was investigated experimentally and numerically in a channel-flow configuration at fuel-rich equivalence ratios ranging from 2 to 7, pressures up to 5 bar and wall temperatures 760–1200 K. Experiments involved in situ one-dimensional Raman measurements of major gas-phase species concentrations over the catalyst boundary layer and planar laser induced fluorescence (LIF) of the OH radical, while simulations included an elliptic 2-D model with detailed heterogeneous and homogeneous reaction mechanisms. The employed reaction schemes reproduced the measured catalytic reactant consumption, the onset of homogeneous ignition, and the post-ignition flame shapes at all examined conditions. Although below a critical pressure, which depended on temperature, the intrinsic gas-phase kinetics of hydrogen dictated lower reactivity for the fuel-rich stoichiometries when compared to fuel-lean ones, homogeneous ignition was still more favorable for the rich stoichiometries due to the lower molecular transport of the deficient oxygen reactant that resulted in modest catalytic reactant consumption over the gaseous induction zone. Above the critical pressure, the intrinsic gaseous hydrogen kinetics yielded higher reactivity for the rich stoichiometries, which resulted in vigorous gaseous combustion at pressures up to 5 bar, in contrast to lean stoichiometry studies whereby homogeneous combustion was altogether suppressed above 3 bar. Computations at fuel-rich stoichiometries in practical channel geometries indicated that homogeneous combustion was not of concern for reactor thermal management, since the larger than unity Lewis number of the deficient oxygen reactant confined the flames to the core of the channel, away from the solid walls. 相似文献
16.
Based on sound speeds in gaseous and liquid air measured by Younglove and Frederick [Int. J. Thermophys. 13(6), 1033-1041 (1992)], empirical equations for the computation of sound speeds in the above media at relatively smaller temperature and pressure ranges were derived. For gaseous air, over a temperature range from 200 to 300 K and pressure from 0.614 to 10.292 MPa, the maximum deviation between the measured sound speeds and those computed with the empirical equation is 56 ppm. For liquid air, over the ranges from 90 to 110 K for temperature and from 0.763 to 13.823 MPa for pressure, the corresponding deviation is 173 ppm. 相似文献
17.
高速飞行器在大气层中飞行时,其光学头罩承受着严重的气动加热。超声速气膜冷却方法可以有效地隔离外部加热,但是冷却气体和主来流形成的混合层会引起光束退化,影响成像质量。为减少光束退化,优化超声速气膜冷却时的光学性能,基于混合层折射率和压力同时匹配设计思路,提出了两种设计方法,即配置特定温度的冷却气体实现混合层折射率和压力同时匹配设计方法和配置特定组分的冷却气体实现混合层折射率和压力同时匹配设计方法,并对设计方法的可行性和有效性进行了验证。模拟证明,后一种方法在外部流动参数不变的情况下,冷却气体的组分构成仅与其喷流静温有关,为气膜的冷却性能和光学性能同步设计奠定了基础。 相似文献
18.
19.
通过衰减全反射(attenuated total reflection,ATR)红外光谱分析与开路热刺激放电(thermally stimulated discharge,TSD)电流、原位实时电荷TSD和电荷等温衰减的测量,研究了氟气对孔洞聚丙烯(PP)膜的氟化改性及氟化改性对其驻极性能的影响.研究结果表明:尽管在负压状态且较低的氟气分压及较低的反应温度(约60℃)和较短的反应时间(约15min)下,氟气能有效地氟化孔洞PP膜,更易于氟化预氧化的孔洞PP膜,氟化改性的孔洞PP膜,尤其是预氧化后的氟化改性
关键词:
孔洞聚丙烯膜
氟气
氟化改性
电荷稳定性 相似文献