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火星上升器倾斜热发射力热效应研究
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作者 熊宗健 赵雨辰 姜毅 《弹箭与制导学报》 北大核心 2025年第2期129-137,I0001,共10页
火星上升器(Mars ascent vehicle,MAV)发射作为火星表面起飞进入环火轨道的第一步,是火星采样返回任务中的关键。MAV倾斜热发射过程力热冲击严重,燃气流动结构复杂,因此设计火星上升器倾斜热发射系统时,必须充分考虑发射过程中复杂的力... 火星上升器(Mars ascent vehicle,MAV)发射作为火星表面起飞进入环火轨道的第一步,是火星采样返回任务中的关键。MAV倾斜热发射过程力热冲击严重,燃气流动结构复杂,因此设计火星上升器倾斜热发射系统时,必须充分考虑发射过程中复杂的力热效应。采用计算流体力学方法,对火星表面MAV倾斜热发射过程的力热冲击效应进行数值模拟研究,并与地球表面环境发射过程对比。研究表明,火星表面MAV斜热发射过程上升器表面最高温度达到2 868 K;发射平台最高温度为2 908 K;MAV出筒过程中,发射平台抬头力矩逐渐增大,在火星低重力环境下,发射装置容易倾覆。火星、地球表面环境倾斜热发射过程差异大,相比于地球表面热发射过程,火星表面MAV发射过程更加稳定,但对平台和上升器力热冲击更加恶劣。 展开更多
关键词 火星采样返回 倾斜发射 数值模拟 冲击
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小型数控车床热态性能的分析优化与实验辨识 被引量:3
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作者 顾庭瑞 《机械设计与制造》 北大核心 2012年第1期164-166,共3页
针对CMK系列小型数控车床运行过程中普遍存在的主轴"翘头"问题,试图通过热变形分析与实验辨识相结合的方法找出上述问题的成因,并给出相应的优化方案,因此,建立了基于有限元法的机床热态特性分析模型来解析整机温度场,同时,... 针对CMK系列小型数控车床运行过程中普遍存在的主轴"翘头"问题,试图通过热变形分析与实验辨识相结合的方法找出上述问题的成因,并给出相应的优化方案,因此,建立了基于有限元法的机床热态特性分析模型来解析整机温度场,同时,通过热应力耦合分析预测了机床各部分的热变形以及主轴的热倾斜,随后,利用红外热成像仪测量、验证了整机温度分布,通过特别设计的六个测点三个方向的热变形实验辨识了主轴系统的热倾斜特性,最后,以降低主轴热倾斜角为目标,给出了提升机床热态性能的两种方案,热优化设计和采用人造花岗岩床身。 展开更多
关键词 数控车床 变形 热倾斜 实验辨识
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Maximum heat transfer capacity of high temperature heat pipe with triangular grooved wick 被引量:4
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作者 沈妍 张红 +2 位作者 许辉 于萍 白穜 《Journal of Central South University》 SCIE EI CAS CSCD 2015年第1期386-391,共6页
A mathematical model was developed to predict the maximum heat transfer capacity of high temperature heat pipe with triangular grooved wick. The effects of the inclination angle and geometry structure were considered ... A mathematical model was developed to predict the maximum heat transfer capacity of high temperature heat pipe with triangular grooved wick. The effects of the inclination angle and geometry structure were considered in the proposed model.Maximum heat transfer capacity was also investigated experimentally. The model was validated by comparing with the experimental results. The maximum heat transfer capacity increases with the vapor core radius increasing. Compared with the inclination angle of0°, the maximum heat transfer capacity increases at the larger inclination angle, and the change with temperature is larger. The performance of heat pipe with triangular grooved wick is greatly influenced by gravity, so it is not recommended to be applied to the dish solar heat pipe receiver. 展开更多
关键词 high temperature heat pipe triangular grooved wick heat transfer capacity
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Effects of turbulator shape,inclined magnetic field,and mixed convection nanofluid flow on thermal performance of micro-scale inclined forward-facing step 被引量:2
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作者 E.JALIL G.R.MOLAEIMANESH 《Journal of Central South University》 SCIE EI CAS CSCD 2021年第11期3310-3326,共17页
This investigation numerically examined the combined impacts of different turbulator shapes,Al_(2)O_(3)/water nanofluid,and inclined magnetic field on the thermal behavior of micro-scale inclined forward-facing step(M... This investigation numerically examined the combined impacts of different turbulator shapes,Al_(2)O_(3)/water nanofluid,and inclined magnetic field on the thermal behavior of micro-scale inclined forward-facing step(MSIFFS).The length and height for all turbulators were considered 0.0979 and 0.5 mm,respectively,and the Reynolds number varied from 5000 to 10000.In order to compare the skin friction coefficient(SFC) and the heat transfer rate(HTR)simultaneously,the thermal performance factor parameter(TPF) was selected.The results show that all considered cases equipped with turbulators were thermodynamically more advantageous over the simple MSIFFS.Besides,using Al_(2)O_(3)/water nanofluid with different nanoparticles volume fractions(NVF) in the presence of inclined magnetic field(IMF)increased HTR.With an increment of NVF from 1% to 4% and magnetic field density(MFD) from 0.002 to 0.008 T,HTR and subsequently TPF improved.The best result was observed for MSIFFS equipped with a trapezoidal-shaped turbulator with 4% Al_(2)O_(3) in the presence of IMF(B=0.008 T).The TPF increased with the augmentation of Re,and the maximum value of it was 5.2366 for MSIFFS equipped with a trapezoidal-shaped turbulator with 4% Al_(2)O_(3),B=0.008 T,and Re=10000. 展开更多
关键词 microchannel forward-facing step TURBULATOR inclined magnetic field heat transfer enhancement
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Effects of wall thickness and material on flame stability in a planar micro-combustor 被引量:1
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作者 LIU Lei ZHAO Liang FAN Ai-wu 《Journal of Central South University》 SCIE EI CAS CSCD 2019年第8期2224-2233,共10页
Flame is prone to lose its stability in micro-combustors due to the large amount of heat loss from the external walls. On the other hand, heat recirculation through the upstream combustor walls can enhance flame stabi... Flame is prone to lose its stability in micro-combustors due to the large amount of heat loss from the external walls. On the other hand, heat recirculation through the upstream combustor walls can enhance flame stability. These two aspects depend on the structural heat transfer, which is associated with the thickness and thermal conductivity of the combustor walls. In the present study, the effects of wall thickness and material on flame stability were numerically investigated by selecting two thicknesses (δ=0.2 and 0.4 mm) and two materials (quartz and SiC). The results show that when δ=0.2 mm, flame inclination occurs at a certain inlet velocity in both combustors, but it happens later in SiC combustor. For δ=0.4 mm, flame inclination still occurs in quartz combustor from a larger inlet velocity compared to the case of δ=0.2 mm. However, flame inclination in SiC combustor with δ=0.4 mm does not happen and it has a much larger blowout limit. Analysis reveals that a thicker wall can enhance heat recirculation and reduce heat loss simultaneously. Moreover, SiC combustor has larger heat recirculation ratio and smaller heat loss ratio. In summary, the micro-combustor with thicker and more conductive walls can harvest large flame stability limit. 展开更多
关键词 MICRO-COMBUSTOR flame stability flame inclination blowout limit heat recirculation heat loss
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