Axial Temperature Behavior of a Heat Exchanger Tube for Microwave Thermal Rockets
Axial Temperature Behavior of a Heat Exchanger Tube for Microwave Thermal Rockets
复制标题
微波热火箭热交换器管的轴向温度行为
DOI：
10.2514/1.27847
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发表时间：
2007
影响因子：
1.9
通讯作者：
M. Barmatz
中科院分区：
文献类型：
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作者：
A. Bruccoleri;K. Parkin;M. Barmatz
A = 通道横截面积 cp T = 恒压比热 D = 通道直径 H T = 对流换热系数 k T = 流体导热系数 l = 通道长度 _ m = 质量流量 Nu = 努塞尔数 P = 内通道周长 Pr = 普朗特数 q00 对流 = 对流热通量 q00 辐射 = 辐射热通量 qtube = 热速率 Re = 雷诺数 Tm = 平均流体温度 Tw = 壁温 T1 = 环境温度 um = 平均值流体速度 " = 发射率 T = 粘度 = 密度 = 斯蒂芬-玻尔兹曼常数
A = channel cross sectional area cp T = specific heat at constant pressure D = channel diameter H T = convective heat transfer coefficient k T = fluid thermal conductivity l = channel length _ m = mass flow rate Nu = Nusselt number P = inner channel perimeter Pr = Prandtl number q00 convection = convective heat flux q00 radiation = radiation heat flux qtube = heat rate Re = Reynolds number Tm = mean fluid temperature Tw = wall temperature T1 = ambient temperature um = mean fluid velocity " = emissivity T = viscosity = density = Stephan–Boltzmann constant
DOI：
--
发表时间：
2009
期刊：
Journal of Propulsion and Power 25(1)
影响因子：
--
作者：
Oda;Y. ;Shibata;T. ;Komurasaki; K. ;Takahashi;K. ;Kasugai;A. ;Sakamoto;K
通讯作者：
K