现在我们有了一个联系，这些绝热过程中，体积比的关系式。
So now we have a relationship between the ratios of these volumes that are reached during these adiabatic paths.
这个绝热过程的温度是,比T1低，因为这是个膨胀过程。
T2 So this is an isotherm at some different temperature T2, a cooler temperature, because this was an expansion.
化学计量比、烟气绝热饱和温度值、喷雾轮切向速度等因素，对脱硫的影响很大。
Flue gas out-let temperature approcich to adiabatic saturation temperature and tangential velocity of spray whool etc.
对于静态、绝热吸积流，比能量E、比角动量L和质量吸积率M都是空间的常量。
For a stationary, adiabatic flow the specific energy E, specific angular momentum L and mass accretion rate M are constant in space.
采用传热传质类比的方法，对多斜孔壁气膜冷却的绝热温比进行了实验研究。
Using the method of heat-mass transfer analogy, experimental research was carried on to investigate adiabatic film effectiveness of inclined multi-hole full-coverage film cooling.
分析了空气比热容比测定实验的系统误差，提供一种对“绝热膨胀过程”中由于不完全绝热而引起的系统误差进行修正的实验方法。
The system errors in the experiment of measuring air specific heat ratio was analyzed and the experimental method for correction was presented.
提出用钢的强度与热导率的比值(强导比)来表征钢的绝热剪切敏感性。
A ratio of strength to thermal conductivity is proposed to characterize the adiabatic shearing sensitivity for steels.
通过数值计算研究超绝热燃烧的形成、以及弥散效应、当量比和多孔介质材料本身对超绝热燃烧特性的影响。
The influences of reaction mechanisms, radiation models, dispersion effects, and variations of physical, thermal and transport properties on numerical results are discussed in detail.
通过数值计算研究超绝热燃烧的形成、以及弥散效应、当量比和多孔介质材料本身对超绝热燃烧特性的影响。
The influences of reaction mechanisms, radiation models, dispersion effects, and variations of physical, thermal and transport properties on numerical results are discussed in detail.
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