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An evaluation of the second order constitutive relations for rarefied gas dynamics based on the second law of thermodynamics.

机译:基于热力学第二定律的稀有气体动力学的二阶本构关系的评估。

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In recent years there has been a resurgence of interest in using the Burnett constitutive equations to describe rarefied flows in which the Navier-Stokes equations no longer provide an accurate approximation. Applications of the Burnett equations have met with some success when used for calculating one-dimensional shock waves and two-dimensional hypersonic blunt body flows. Accurate solutions for more complex flows, however, have been elusive. The original objective of this research was to apply the Burnett equations to the cowl lip shock interaction problem associated with the engine inlet of hypersonic air-breathing vehicles. However, during the course of the investigation, it was discovered that the Burnett equations may fail to satisfy the second law of thermodynamics.; The entropy balance relation for the Burnett equations is constructed from two points of origin. It is first derived from classical thermodynamic theory using the Gibbs equation and the continuum conservation relations for mass, momentum and energy. A similar relation is also derived from kinetic theory using Boltzmann's H-theorem in conjunction with the Chapman-Enskog expansion. The entropy source appearing in the balance relations is found to be negative for certain situations, in violation of the second law of thermodynamics. Numerical simulations of one- dimensional shock waves are used to support this conclusion.; Moreover, the two derivations are shown to be completely equivalent to second order in the Knudsen number, indicating that the Gibbs equation is indeed compatible with the Burnett equations, contrary to common understanding. The implications are such that neither the classical Gibbs equation, nor the Burnett equations, is adequate to describe the effects of translational non-equilibrium. A better continuum approach to modeling a non-equilibrium gas might include an expanded set of thermodynamic variables and the corresponding relaxation equations. The Burnett equations do not accomplish this. However, the 13-moment approximation of Grad and the relatively new discipline of extended irreversible thermodynamics may offer such an alterative.
机译:近年来,人们开始重新关注使用伯内特本构方程来描述稀疏流的问题,在这种稀疏流中,Navier-Stokes方程不再提供精确的近似值。当用于计算一维冲击波和二维高超音速钝体流时,Burnett方程的应用取得了一些成功。但是,对于更复杂的流的精确解决方案却难以捉摸。这项研究的最初目的是将Burnett方程应用于与超音速吸气飞行器的发动机进气口相关的前唇冲击相互作用问题。然而,在研究过程中,发现伯内特方程可能无法满足热力学第二定律。 Burnett方程的熵平衡关系是从两个原点构建的。它首先是从经典热力学理论出发,使用吉布斯方程和质量,动量和能量的连续性守恒关系得出的。使用玻耳兹曼H定理结合查普曼-恩斯科格展开式的动力学理论也得出了类似的关系。发现在平衡关系中出现的熵源在某些情况下是负的,这违反了热力学第二定律。一维冲击波的数值模拟被用来支持这一结论。此外,这两个推导被显示为完全等效于Knudsen数的二阶,这表明Gibbs方程确实与Burnett方程兼容,这与通常的理解相反。这样的含义使得经典的吉布斯方程和伯内特方程都不足以描述平移非平衡的影响。对非平衡气体进行建模的更好的连续方法可能包括扩展的热力学变量集和相应的弛豫方程。 Burnett方程式不能完成此任务。但是,Grad的13矩近似和扩展的不可逆热力学的相对较新的学科可能提供了这种替代方法。

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