I'm going to go to the second one, which is the effect of the total pressure on the reaction.
来看第二个，总压强对反应的影响。
Because really what we want is the total pressure as a function of the composition in the gas phase.
因为我们想要的是，总压强作为气相组分的函数。
The question we're going to ask is, what happens when we change the total pressure in this reaction here.
我们要问的问题是，总压强改变时，会发生什么事。
Such that the sum of the partial pressure of the inert gas, plus the partial pressure of A, is the total pressure. One bar, in our case.
总压强P等于惰性气体的分压，与A物质的蒸汽压之和，在我们的例子中总压强是一个大气压。
And blowers are chosen according to calculation of air volume and total pressure loss.
风机根据计算空气量和总压力损失的数值进行选择。
Outlet total pressure and volume flow are the main indexes of a pneumatic extinguisher.
风力灭火机的主要技术指标是出口全压与风量。
The total pressure of mixed gas equals to the summation of partial pressure of each composition.
混合气体的总压力是各组成气体的分压力的总和。
A novel method was proposed based on the total pressure of pitot tube and power spectral density.
通过分析皮托管动压信号的方式，提出了一种基于功率谱密度分布的调节阀扰动信号分析新方法。
It is shown that the U-bottom orifice has higher total pressure drop and (thermodynamic) efficiency.
结果表明，U型弧底节流孔具有更大的压降和更高的热力学效率。
The more convergence Angle increases, the greater dynamic pressure, static pressure and total pressure rise.
当合流角增加时，动压、静压、全压均会增大，且角度越大增幅越明显。
The shock total pressure was estimated with the normal component of the Mach number using normal shock theory.
激波总压损失用正激波关系式通过马赫数法向分量估计。
The technique of the lip with cut-out can be used to simulate exactly the shape of the total pressure contour map.
采用圆弧切割法能较正确地模拟总压等值线形状。
The results show that this type of inlet has high total pressure recovery coefficients at a wide range of yaw angle.
研究表明，该类进气道在各种侧滑状态下总压恢复系数较高。
The numerical calculated method was used to research the technology of the total pressure distortion with flashboard.
本文通过数值计算的方法研究插板式总压畸变试验技术。
The results show that the transmittances of the films are higher and higher with the sputtering total pressure increase.
由试验可知，薄膜透过率随溅射气体总压的升高而升高。
The maximization of the static pressure rise and minimization of the total pressure loss are taken as the design targets.
压气机叶型气动优化设计目标是静压升最大和总压损失最小。
The static pressure distribution is similar to the total pressure, and they all show symmetry along the radius direction.
静压和总压的分布规律比较相近，沿半径方向的分布呈现较好的轴对称性。
Variation histories of total pressure of the vacuum system, product temperature as well as product mass are achieved by numerical calculation.
通过数值解算得到系统总压、产品温度(表面温度、中心温度、质量平均温度)、产品质量随时间的变化曲线。
The effect of the velocity difference on total pressure loss may be neglected, if the density and the static temperature difference are equal.
若密度比、静温比相同或相近时，速度差对总压损失的影响可忽略。
Hence, the method of vortex control is available for removing swirl, decreasing total pressure loss, and improving flow field in S-shaped intake.
因此，抽气形式的有源涡控是抑制旋流、减少出口总压平均损失、改善S弯进气道出口流场的有效措施。
Moreover, the separation zone is only a low-energy fluid gathering area for large total pressure loss and entropy rather than a zone of loss source.
分离区仅是高总压损失和高熵值的低能流体聚集区，而非高损失来源区；
According to the different motor ignition states, a series of total pressure values of observed points on the respective jet axis distances was measured.
针对不同的发动机点火状态，在射流轴线的不同距离上对一系列测点位置的总压参数进行了测量。
After optimization, the total pressure loss of the turbine vane was reduced by 0.95%, and the efficiency of the overall compressor was increased by 2.1%.
经优化后，透平高压级静叶的总压损失系数减少0.95%；多级压气机整机效率提高2.1%。
Due to the smaller Angle of injection, the ratio of total pressure loss of aerodynamic ramp is less than the physical ramp and transverse injection stream.
由于喷流方向与主流方向夹角较小，总压损失也较物理斜坡、横向喷流等混合增强方式小。
Characteristics and influence factors of total pressure distortion are studied based on tests conducted on a disturbed board installed in the nacelle inlet.
在吊舱进气道进口安装扰流板进行试验，研究扰流板进气畸变的影响因素及总压畸变特征。
Test results show lower exit average total pressure recovery, larger circumferential total pressure distortion and stronger and more irregular secondary flow.
试验表明其出口平均总压恢复系数较低，周向总压畸变指数较大，旋流较强且很不规则。
The section average total pressure and the average total pressure in the circumferential low-pressure areas are in linear relationship with the air inlet flow.
截面平均总压和周向低压区内平均总压与进气流量成线性关系。
The section average total pressure and the average total pressure in the circumferential low-pressure areas are in linear relationship with the air inlet flow.
截面平均总压和周向低压区内平均总压与进气流量成线性关系。
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