| 1. | The maximum wall heat transfer rates generally occur at the throat .
壁的最大热交换率通常发生在喉部处。 |
| 2. | Usually, it also causes the wall heat transfer rate to decrease somewhat in the region downstream from the point of separation .
通常，它也会使分离点下游区间内的壁热交换率有所减少。 |
| 3. | Standard test method for measuring heat transfer rate using a thin - skin calorimeter
用薄皮热量计测量传热速率的标准试验方法 |
| 4. | Test method for calibration of heat transfer rate calorimeters using a narrow - angle blackbody radiation facility
用窄角黑体辐射设备校准传热速度量热器的方法 |
| 5. | The total heat transfer rate , including sensible and latent heats , and sensible heat factor are obtained by experiment
由实验结果发现，湿盘管有水凝结现象的发生。 |
| 6. | The test results indicate that the heat transfer rates of the test coils increase with air inlet velocity and fin numbers
由实验数据得知湿盘管总热传量中，潜热量的变化占了大部分。 |
| 7. | In addition , the heat transfer rate and the ability of dehumidification for slit - fin - type heat exchangers are superior to the plain - fin - type coils
此外，裂口鳍片型式的热传量及除湿率均高于平板鳍片型式的热交换器。 |
| 8. | It is analyzed that the thermal and chemical model have a effect on the shock detached distance , heat transfer rate , the distributions of temperature and density
分析了各种气体模型对激波脱体距离、壁面热流、温度分布和密度分布等的影响。 |
| 9. | Finally , three foundational principles are presented for the optimal design of the fin system with lower flow resistance and higher heat transfer rate
在此基础上，提出并理论证明了低阻力高传热的翅片结构的优化设计应遵循的三个基本原则。 |
| 10. | The results of analysis show that the shock detached distance computed by two temperature model or three temperature compare well with the experiment data , and the heat transfer rate is highest for one temperature model with non - catalytic wall , and lowest for equilibrium gas model , and the heat transfer rate for perfect gas model is between the non - catalytic wall and fully catalytic wall
结果表明：采用两温度（或三温度）非平衡气体模型计算的激波脱体距离更接近实验情况；采用平衡气体模型计算的壁面热流最高，一温度非平衡气体模型完全非催化的壁面热流最低，而完全气体模型的壁面热流在两者之间。 |
