考虑到气体温度变化，给出了对校准压力进行温度修正的方法。
It deduced the way to do the temperature corrections in calculating calibration pressure when considering the gas temperature change.
对问题的产生原因和机理进行分析，认为问题的产生原因可能在于方波压力上升沿导致的被测气体温度变化。
On the basis of the mechanism analysis of the problem, the temperature rise of the measured medium caused by step pressure could lead...
当工作气体温度变化时，脉冲TEA CO_2激光器的输出波长也可能发生变化，此现象称为输出波长的温度漂移。
The output wavelength would change according to the change of the temperature of the gas mixture in a pulsed TEA CO_2 laser, which is called the wavelength-temperature shift.
进行三个脉冲管与行波型热声发动机的配合实验，着重研究了热端气体温度、冷端温降和压力振幅的变化规律。
The experiment focuses on the temperature of the gas in the hot end heat exchanger, the temperature decline of the cold end of the pulse tube and pressure amplitude.
气体经喷嘴进入聚合物熔体时所形成的气熔界面的运动情况随着进气压力、熔体温度等不同参数的改变而发生变化。
The interface motion situation of gas-melt is changed when injecting gas into melt in various conditions-gas-entering pressure, melt temperature and so on.
采用实验方法研究了干熄炉内焦炭的冷却过程，得到了实验条件下不同位置焦炭的冷却曲线和气体温度、压力损失的变化趋势。
The coke cooling process in the coke dry quenching shaft furnace was investigated experimentally. The coke and gas temperatures and the pressure drop were measured.
当气体从高压到低压在等熵下膨胀时所产生的气体温度的变化。
The change in gas temperature that occurs when the gas is expanded at constant enthalpy from a high to low pressure.
航空发动机控制系统半物理模拟试验中，涡轮出口气体温度高、变化快，难以模拟。
In the matter - in - loop simulation experiment of aero - engine control system, the turbine outlet temperature, which characteristics with high and quick change , is hard to be simulated.
航空发动机控制系统半物理模拟试验中，涡轮出口气体温度高、变化快，难以模拟。
In the matter - in - loop simulation experiment of aero - engine control system, the turbine outlet temperature, which characteristics with high and quick change , is hard to be simulated.
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