Repetitively Pulsed Hypersonic Flow Apparatus for Diagnostic Development
Repetitively Pulsed Hypersonic Flow Apparatus for Diagnostic Development
复制标题
用于诊断开发的重复脉冲高超声速流量仪
DOI：
--
复制
发表时间：
2012
期刊：
影响因子：
--
通讯作者：
S. North
中科院分区：
文献类型：
--
作者：
R. Sánchez‐González;R. Srinivasan;Jerrod W. Hofferth;Doyong Kim;Andrew Tindall;R. Bowersox;S. North
Cp = 定压热容 Cv = 定容热容 C12 = 实验确定的校准常数 De = 喷嘴出口直径 Ds = 喷嘴亚音速部分直径 Dt = 喷嘴喉部直径 k = 玻尔兹曼常数 M = 马赫数 m = 质量 Pi = 冲击压力 P0 = 停滞压力 P02 = 皮托管压力 Sf = 荧光信号强度 Trot = 旋转温度 Tw = 壁温 T0 = 停滞温度 = 热容量比，Cp=Cv E21 = 旋转状态之间的能量差
Cp = heat capacity at constant pressure Cv = heat capacity at constant volume C12 = experimentally determined calibration constant De = exit diameter of nozzle Ds = diameter of subsonic section of nozzle Dt = throat diameter of nozzle k = Boltzmann constant M = Mach number m = mass Pi = impact pressure P0 = stagnation pressure P02 = pitot pressure Sf = fluorescence signal intensity Trot = rotational temperature Tw = wall temperature T0 = stagnation temperature = ratio of heat capacities, Cp=Cv E21 = energy difference between rotational states
脉冲超声束中的稳态流动条件
DOI：
10.1063/1.4824155
发表时间：
2013
期刊：
The Journal of chemical physics
影响因子：
--
作者：
Wolfgang Christen
通讯作者：
Wolfgang Christen