共查询到20条相似文献,搜索用时 171 毫秒
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建立了热管废热锅炉的换热器模型,研究了在各种管排组合方案下的分离式热管换热器的工质温度分布、管壁温度分布、烟气温度分布及热回收量等,结果表明,调整管排组合是解决工质温度过高和低温腐蚀问题的一种有效方法. 相似文献
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在长度为20 cm的石英毛细管内利用两个边缘锋利的中空的针型电极之间的氩气放电产生了高电子密度的大气压等离子体。利用发射光谱对所获得的等离子体的几个重要参数进行了诊断。利用计算机谱线拟合法合成了300 nm附近OH(A-X)的(0-0)转动谱带并通过与测量谱线的比较确定了等离子体的气体温度,根据Hβ谱线Stark展宽法计算了等离子体的电子密度,采用玻尔兹曼曲线斜率法依据测得的有关氩的发射光谱估算了等离子体的电子温度。研究结果表明,这种石英毛细管内弧光放电等离子体的气体温度约为(1 100±50)K;电子密度数量级在1014 cm-3;电子温度约为(14 515±500)K。 相似文献
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赵纪军 《原子与分子物理学报》2008,25(6)
应用第一性原理密度泛函理论计算了MgO在零温(0K)下和0~200GPa静水压范围内的晶体结构和弹性模量,以及B1、B4和B8相结构的MgO的声速随压力的变化。利用准简谐近似下的Debye模型,通过拟合三阶Birch-Murnaghan物态方程模拟了高温效应并对三个相在高温高压下的相稳定性做了研究。本工作的计算结果与前人的理论和实验结果符合较好,说明第一性原理结合准简谐Debye模型能够比较准确的模拟矿物如MgO在高温高压下的热力学性质。 相似文献
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MgO高温高压特性及相变的第一性原理研究 总被引:1,自引:1,他引:0
应用第一性原理密度泛函理论计算了MgO在零温(0K)下和0~200GPa静水压范围内的晶体结构和弹性模量,以及B1、B4和B8相结构的MgO的声速随压力的变化。利用准简谐近似下的Debye模型,通过拟合三阶Birch-Murnaghan物态方程模拟了高温效应并对三个相在高温高压下的相稳定性做了研究。本工作的计算结果与前人的理论和实验结果符合较好,说明第一性原理结合准简谐Debye模型能够比较准确的模拟矿物如MgO在高温高压下的热力学性质。 相似文献
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A new approach to describe phenomena attendant on the growth of thin InGaAs epitaxial layers by hydride MOCVD in terms of which the boundary gas layer is considered as quasi-liquid is suggested. A numerical model for simulating the concentration profiles of the components in quantum-well heterostructures is developed. It is based on the assumption that a state close to thermodynamic equilibrium exists near the interface. The concentration profiles are simulated by jointly solving equations that describe heterogeneous equilibria and material balance at the interface. The indium profiles in InGaAs/GaAs quantum-size heterostructures are simulated at various parameters of the epitaxy process, such as temperature, initial component ratio in the gas phase, and boundary layer thickness. The results obtained agree well with the available experimental data. 相似文献
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Numerical analysis of the effects of radiation heat transfer and ionization energy loss on the cavitation Bubble?s dynamics 总被引:1,自引:0,他引:1
A numerical scheme for simulating the acoustic and hydrodynamic cavitation was developed. Bubble instantaneous radius was obtained using Gilmore equation which considered the compressibility of the liquid. A uniform temperature was assumed for the inside gas during the collapse. Radiation heat transfer inside the bubble and the heat conduction to the bubble was considered. The numerical code was validated with the experimental data and a good correspondence was observed. The dynamics of hydrofoil cavitation bubble were also investigated. It was concluded that the thermal radiation heat transfer rate strongly depended on the cavitation number, initial bubble radius and hydrofoil angle of attack. 相似文献
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氧气放电等离子体温度测量研究 总被引:1,自引:0,他引:1
为了考察电激励氧碘激光器中放电腔内的宏观气体温度,由两片蚌形铜电极和一根长30 cm内径1.65 cm的耐热玻璃管构成放电腔装置,用一台最高功率500 W,频率13.56 MHz的射频装置对压力1 330Pa的纯氧气体进行了介质阻挡放电研究。利用O2(b,ν=0)的P支发射光谱,分别采用波尔兹曼直线作图法和计算机模拟发射光谱法,测量了氧气射频放电等离子体的宏观气体温度。对于低分辨率光谱,利用高斯拟合进行了分峰处理,利用峰面积表征发光强度,通过波尔兹曼作图法得到了宏观气体温度。利用氦氖激光器测得的光谱仪狭缝函数获得了计算1机模拟发射光谱,以最小二乘法作为判据,通过比较计算机模拟发射光谱和实测光谱获得了宏观气体温度。 相似文献
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Yutaka Wada Yoshio Seike Nobuyuki Tsuboi Katsuya Hasegawa Kiyokazu Kobayashi Makihito Nishioka Keiichi Hori 《Proceedings of the Combustion Institute》2009,32(2):2005-2012
Tetra-ol glycidyl azide polymer (GAP) is one of the best candidates for the solid fuel of gas hybrid rocket system because of self-combustibility, better mechanical property and high heat of formation, and comprehensive understanding of combustion phenomena is indispensable for such an application. Combustion model of GAP, which is one-dimensional three-phase mode combustion model, was developed by Beckstead et al. and they applied it to tri-ol GAP successfully. We have applied this model to tetra-ol GAP as an initial attempt, and numerical simulation showed that maximum temperatures in the gas phase exceeded those of experimental results significantly, and calculated burning rates were much higher than strand burner data, thus, modification of the model taking account of combustion incompleteness was found to be necessary. Combustion residues of GAP were investigated, and those were found to be composed of soot (black color), and high viscosity residue (HVR), and yellow powder which was only observed at high pressures. These residues were analyzed by means of SEM and FTIR, and mass balance was also measured. Modifications of combustion model were made taking the residue analysis results into account as Blow Off Mechanism. Simulated final temperature in the gas phase and burning rate are lowered effectively and coincide well with experimental data adjusting kinetic parameters. 相似文献
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通过表面形貌观察、温度场分析,研究了切向空气气流、切向氮气气流、自然对流3种环境下氟化氘(DF)激光对45#钢靶的辐照效应,结果表明:切向空气气流环境下,钢靶烧蚀效果最显著,靶板后表面中心温升最高;切向氮气气流环境下,钢靶有一定的烧蚀,但温升最低;自然对流环境下,烧蚀效果最差。实验结果表明:切向气流可移除部分熔化物,特别在切向空气气流环境下剧烈的氧化反应可促进钢靶温度升高,显著增强激光对钢靶的烧蚀,停止激光辐照后切向气流的冷却效应起主要作用。根据实际物理问题建立了相应的数值计算模型,模拟了不同气流环境下激光对钢靶的辐照效应,其中,利用"生死单元"的方法,模拟了切向空气气流环境下激光对钢靶的烧蚀,并考虑了氧化放热的影响。模拟结果与实验结果基本相符,解释了气流在激光辐照效应中的作用。 相似文献
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综合考虑高功率微波对电子的加速过程以及电子与气体分子的碰撞过程,建立了单一气体与混合气体击穿过程的蒙特卡罗仿真模型,编写了三维蒙特卡罗仿真程序(3D-MCC)。针对单一气体Ar和N2以及混合气体N2/O2展开研究,仿真了气体雪崩击穿电子云形成过程,对比分析了不同气体电子能量分布函数随压强的变化规律。发现了Ar击穿特性受电子能量分布函数影响较大,而N2击穿特性受电子能量分布函数影响较小。通过分析平均电子能量以及电子密度随时间的变化过程,得到了Ar和N2击穿时间,并通过与流体模型计算得到的击穿时间比对分析验证了3D-MCC模型的正确性。在真空腔体内开展了S波段高功率微波大气击穿实验,测量得到了场强为6.38 kV/cm时不同压强下的大气击穿时间。通过在辐射源与真空腔体之间增加聚焦透镜,大大减小了壁效应的影响,并且采用模型仿真得到的大气击穿时间与实验结果吻合较好。 相似文献
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对双温模型的重要热学参量电子热容、电子弛豫时间、电子热导率进行量子化处理,使双温模型能适用于自由电子温度比较高的情况.利用前向差分算法,数值求解了电子-晶格双温双曲两步热传导模型,所得的结果更接近实验值.经过分析得出: 1)薄膜前表面自由电子温度达到最大值的时间约为0.27 ps,得到的损伤阈值与实验值符合较好.2)电子热容对电子温升规律影响非常大.电子热导率对自由电子温升规律也有较大的影响.3)在趋肤层内自由电子温升非常快,不同厚度自由电子温度达到最大值所需的时间延迟不明显.趋肤层以下自由电子温度升高较慢,不同厚度自由电子达到最大值所需的时间延迟明显. 相似文献