Navier-Stokes方程(NSE)的物理与数学问题

Q2 Engineering
H. Dumitrescu, V. Cardoş, Radu Bogateanu
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引用次数: 0

摘要

描述粘性/实流体在Rn (n = 2或3)中的运动的Navier-Stokes方程通过雷诺数依赖于一个正系数(粘度,ν)。NSE问题的关键是雷诺数,它在数学上被认为是一个没有任何物理解释的简单的小扰动参数,或者是一个模糊的物理牛顿惯性力与粘性力之比,𝑅𝑅𝑅𝑅=𝑈𝑈𝑈𝑈𝑈𝑈𝑈𝑈,尽管它的定量物理意义是运动开始时(t = 0时的IC)的初始激励与响应比。但随着雷诺数的增加,它并不趋于零(ν→0),保持一个有限值,与新的热力学平衡态相对应。对于Re→∞,(ν→0)假物理条件使得NSE问题的唯一解小于一个超过临界雷诺数Recr。在小尺度(慢运动,小Re)和大尺度(湍流运动,大Re)下,对壁面有界粘性流动的理解必须与壁面在启动阶段对固有流体动力学的“壁面”滞后概念的更微妙的扭转屈曲效应结合起来。在运动开始时,与acr/g≥2/3量级的启动加速度相关的绝热壁的限制,为NSE解的数学唯一性的丧失创造了物理条件(热分子变化)。在续文中,结合NSE模型的有效性区域,考虑了物理限制。由于偏微分方程的非线性,几何和物理性质的变化可能导致解的分岔,从而导致多解。对于与壁面或多或少接触的流动流体的分子结构变化所产生的更复杂的溶液结构,层流-湍流过渡作为主要分岔源的考虑,给出并说明了平板上的典型流动和启动/接触涡(“涡眼”)的粘性衰减。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
The Physical vs. Mathematical Problem of Navier-Stokes Equations (NSE)
The Navier-Stokes equations describing the motion of viscous/real fluids in Rn (n = 2 or 3) depend on a positive coefficient (the viscosity, ν) via the Reynolds number. The key of NSE problem is the Reynolds number, mathematically considered a simple small perturbation parameter without any physical explanation, or a vague physical Newtonian ratio of inertial to viscous forces, 𝑅𝑅𝑅𝑅=𝑈𝑈𝑈𝑈𝜈𝜈, in spite of its quantic physical meaning as the initial excitation to response ratio, at the beginning of motion (IC at t = 0). The paper deals with the thixotropic property of real viscosity which softens (ν ↓) when strained (Re↑), but it doesn’t tend to zero (ν → 0) as much as the Reynolds number increases, holding a finite value, corresponding to the new thermodynamic equilibrium state. The (ν → 0 for Re → ∞) false physical condition renders the NSE problem to a unique solution less one beyond a critical Reynolds number, Recr. The understanding of the wall-bounded viscous flows, at both small-scales (slow motion, small Re) and larger scale (turbulent motion, large Re) must be in conjunction with the more-subtle torsional buckling effect of the “wall” lag concept that the wall has on the inherent fluid dynamics during the starting phase. The limitations of the diathermal wall associated with the starting accelerations at the onset of motion, of the order of acr/g ≥ 2/3, create the physical conditions (thermomolecular changes) for the loss of the mathematical uniqueness of the NSE solutions. The physical limitations in conjunction with the validity area of NSE model are considered in the sequel. Because of the nonlinearity of the PDE differential equations, the variation of geometrical and physical properties can lead to bifurcations in the solution and thus, to multiple solutions. Considerations relative to laminar-turbulent transition as the main bifurcation source for the more complex structure of a solution, engendered by molecular structure changes of a flowing fluid in more or less contact with the walls, are given and illustrated for the canonical flows on flat plates and viscous decay of a starting/contact vortex (“vortex eye”).
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来源期刊
INCAS Bulletin
INCAS Bulletin Engineering-Aerospace Engineering
自引率
0.00%
发文量
50
审稿时长
8 weeks
期刊介绍: INCAS BULLETIN is a scientific quartely journal published by INCAS – National Institute for Aerospace Research “Elie Carafoli” (under the aegis of The Romanian Academy) Its current focus is the aerospace field, covering fluid mechanics, aerodynamics, flight theory, aeroelasticity, structures, applied control, mechatronics, experimental aerodynamics, computational methods. All submitted papers are peer-reviewed. The journal will publish reports and short research original papers of substance. Unique features distinguishing this journal: R & D reports in aerospace sciences in Romania The INCAS BULLETIN of the National Institute for Aerospace Research "Elie Carafoli" includes the following sections: 1) FULL PAPERS. -Strength of materials, elasticity, plasticity, aeroelasticity, static and dynamic analysis of structures, vibrations and impact. -Systems, mechatronics and control in aerospace. -Materials and tribology. -Kinematics and dynamics of mechanisms, friction, lubrication. -Measurement technique. -Aeroacoustics, ventilation, wind motors. -Management in Aerospace Activities. 2) TECHNICAL-SCIENTIFIC NOTES and REPORTS. Includes: case studies, technical-scientific notes and reports on published areas. 3) INCAS NEWS. Promote and emphasise INCAS technical base and achievements. 4) BOOK REVIEWS.
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