Thermodynamic Properties of Vapors from Speed of Sound

M. Bijedić, S. Begić
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引用次数: 3

Abstract

A numerical procedure for deriving the thermodynamic properties , , and of the vapor phase in the subcritical temperature range from the speed of sound is presented. The set of differential equations connecting these properties with the speed of sound is solved as the initial-value problem in domain . The initial values of and are specified along the isotherm with the highest temperature, at a several values of [0.1, 1.0]. The values of are generated by the reference equation of state, while the values of are derived from the speed of sound, by solving another set of differential equations in domain in the transcritical temperature range. This set of equations is solved as the initial-boundary-value problem. The initial values of and are specified along the isochore in the limit of the ideal gas, at several isotherms distributed according to the Chebyshev points of the second kind. The boundary values of are specified along the same isotherm and along another isotherm with a higher temperature, at several values of . The procedure is tested on Ar, N2, CH4, and CO2, with the mean AADs for , , and at 0.0003%, 0.0046%, and 0.0061%, respectively (0.0007%, 0.0130%, and 0.0189% along the saturation line).
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从声速看蒸汽的热力学性质
给出了一种由声速推导亚临界温度范围内气相热力学性质的数值计算方法。将这些性质与声速联系起来的微分方程组作为定义域上的初值问题求解。和的初始值是沿着最高温度的等温线指定的,在几个值[0.1,1.0]。的值是由参考状态方程得到的,而的值是通过在跨临界温度范围内求解另一组域微分方程由声速得到的。将这组方程求解为初边值问题。和的初值是沿着理想气体极限的等温线,在按第二类切比雪夫点分布的几条等温线上指定的。的边界值沿同一等温线和沿另一条温度较高的等温线指定,在若干值处。该方法在Ar, N2, CH4和CO2上进行了测试,和的平均AADs分别为0.0003%,0.0046%和0.0061%(沿饱和线为0.0007%,0.0130%和0.0189%)。
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