• We plug in all the numbers, and we get that the total pressure is now 0.685 bar.

    把这些数都代入方程,总气压等于0。685巴。

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  • Are we going to try to figure out how the total pressure above the solution changes.

    我们能不能得到溶液上的总气压,是如何变化的。

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  • I'm going to have the total pressure is going to be the partial pressure of the water.

    我先考虑总压强,等于水的蒸汽压的情况。

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  • So I'm going to find the total pressure as a function of the composition in the gas phase.

    我想找到总压强作为,气相中组分的函数。

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  • 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。

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  • 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。

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  • 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。

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  • So now if I draw a diagram, and I just focus on, so there's the total pressure sitting here.

    现在如果我要画相图,我只需要关注,这里代表总压强。

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  • 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。

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  • So let's take the derivative of this with respect to total pressure. Well, this isn't total pressure.

    对这个方程两边对总的压强求导,好,这里不是总压强。

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  • 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。

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  • Tells you the pressure of, the total pressure, or partial pressure at coexistence and the composition.

    告诉我们总压强,共存曲线上分压和组分比。

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  • 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。

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  • 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。

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  • So all the, both of the partial pressures and the total pressure are going to go lower than indicated here.

    那么所有的,两个分压,和总压强会比,这里指示的低。

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  • 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。

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  • 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。

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  • There exist a close coupling relation between the wind tunnel flow field parameters, total pressure and Mach number.

    风洞流场参数—总压、马赫数之间存在严重的耦合关系。

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  • 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。

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  • 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。

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  • 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。

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  • 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。

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  • 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。

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  • For a given media, and at a constant total pressure and temperature, the partial pressure of oxygen is proportional to oxygen mole fraction.

    对一个给定的媒介,在恒定的总压和温度下,局部压力与氧的克分子数成比例。

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  • 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。

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  • 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。

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  • 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。

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  • 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%。

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  • 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。

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  • 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。

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