Boltzmann方程简化计算方法与气固边界条件研究进展

Research progress on simplified computational methods for Boltzmann equation and gas-solid boundary conditions

  • 摘要: 稀薄气体动力学作为连接分子尺度运动与流体输运行为的重要桥梁,在航天器再入飞行、高速气动和微纳尺度输运等领域具有广泛应用。当气体分子平均自由程与流动特征长度可比时,连续介质假设失效,气体非平衡输运效应显著,气固边界处产生速度滑移与温度跳跃现象,此时平衡态分布条件不再成立,经典的Navier–Stokes方程难以准确描述流动。Boltzmann方程作为刻画稀薄气体非平衡输运的基本方程,描述了气体分子输运过程的统计规律,在一定条件下能够描述从自由分子流到连续流的全流域流动现象。为实现对Boltzmann方程的有效求解,国内外学者提出了多种近似建模与简化策略,包括宏观封闭模型、粒子方法与随机模拟、离散速度与介观动理学方法,以及近年来发展的混合算法等。此外,稀薄气体流动另一个关键问题是气固相互作用及其边界条件的建模,从微观、介观到宏观全尺度准确描述气固边界相互作用对于跨流域多尺度流动预示至关重要。本文对近年来国内外在稀薄气体动力学理论方法与气固边界条件建模方面所取得的进展进行梳理和归纳总结,并指出当前稀薄气体动力学研究的核心挑战在于如何有效建立兼顾预示精度与计算成本的Boltzmann简化建模理论及其精度适用的边界条件,对推动稀薄气体动力学的发展并服务于超低轨卫星、深空探测等航天工程应用,具有十分重要的理论与实际工程价值。

     

    Abstract: Rarefied gas dynamics serves as an essential bridge connecting molecular-scale motion to macroscopic fluid transport behavior, with broad applications in spacecraft re-entry flight, hypersonic aerodynamics, and micro/nano-scale transport. When the molecular mean free path becomes comparable to the characteristic flow length, the continuum assumption fails, and significant non-equilibrium transport effects emerge. At gas-solid interfaces, velocity slip and temperature jump occur, where the equilibrium distribution condition no longer holds, and the classical Navier–Stokes equations fail to accurately describe the flow. The Boltzmann equation, as the fundamental governing equation for non-equilibrium rarefied gas flow, describes the statistical laws of molecular transport and, under certain conditions, is capable of capturing flow phenomena across the entire regime from free molecular to continuum flow. To enable efficient solutions of the Boltzmann equation, researchers have proposed various approximate modeling and simplification strategies, including macroscopic closure models, particle-based methods and direct simulation Monte Carlo, discrete velocity methods and mesoscopic gas-kinetic schemes, as well as hybrid algorithms developed in recent years. Another critical issue in rarefied gas flows concerns the modeling of gas–solid interactions and the associated boundary conditions. Accurately characterizing these interactions across micro-, meso-, and macroscopic scales is essential for the predictive simulation of multi-scale flows spanning different regimes. This paper reviews and synthesizes recent progress in both theoretical approaches to rarefied gas dynamics and the modeling of gas–solid boundary conditions. It is further identified that the core challenge in current research lies in effectively establishing simplified Boltzmann formulations and their corresponding boundary conditions that strike a balance between predictive fidelity and computational cost. Addressing this challenge is of substantial theoretical and practical value for advancing rarefied gas dynamics and supporting aerospace engineering applications, including very-low-Earth-orbit satellites and deep-space exploration.

     

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