stagnation temperature

stagnation temperature 基本解释

驻点温度；临界温度

化学

重点词汇

• temperaturen. 温度, 发烧, 热度 [化] 温度
• stagnationn. 淤塞, 停滞 [医] 停滞, 滞留, 郁积

stagnation temperature 双语例句

1. 1、 Fine-wire stagnation temperature probe
   细丝临界温度探测器
2. 2、 The stagnation enthalpy and stagnation temperature are often employed in a thermodynamic cycle.
   在热力循环中，经常使用滞止焓和滞止温度的概念。
3. 3、 The results indicate that the thickness variations exhibit no significant influence on stagnation temperature, while the cooling power drops sharply as the thickness increases.
   计算结果表明：驻点温度随热防护层厚度的变化并不明显，而冷却系统功率随热防护层厚度增加急剧降低；
4. 4、 The stagnation temperature at compressor outlet may be calculated from the stagnation enthalpy of compressor outlet air.
   根据压气机出口空气滞止焓，可以计算压气机出口滞止温。
5. 5、 The effects of the stagnation temperature and stagnation pressure's non symmetrical distribution on the thrust misalignment of conical nozzle
   锥型喷管总温、总压分布不均匀对推力偏心的影响
6. 6、 A stagnation pressure and stagnation temperature were set at the pipe inlet.
   在管路的进口处，给定总压力和总温度。
7. 7、 In the model the exit area ratio, solid particle mass ratio, fuel enthalpy of combustion, jet gas molecular weight, chamber stagnation temperature, flight Math number etc. have been considered.
   在该模型中考虑了底排出口面积比，排气固相颗粒质量比，燃料热值，燃气分子量，燃烧室总温，飞行马赫数等因素。
8. 8、 The experimental results show that autoignition was sensitive to a number of parameters: air stagnation temperature and pressure, and wall configuration of the combustor, The temperature and wall configuration has significant effect on the autoignition.
   发现滞止温度、滞止压力和燃烧室内部构型等都对自燃有影响，特别是滞止温度和内壁构型的影响非常大。
9. 9、 Front stagnation point has the minimum temperature, the rear shoulder has the maximum temperature, the thermal boundary layer in the high temperature significantly increased with the velocity increasing.
   车头驻点处温度最小，车尾肩部温度最大，热边界层内的最高温度随着速度的增大显著升高。
10. 10、 Under different environmental parameters of the gas will certainly be reflected in the inherent and aerodynamic parameters, such as the stagnation pressure, temperature, gas flow.
    不同环境下的的气体参数，肯定会反映在与空气动力本身固有的参数上，如滞止压强，温度，气体流量等。