飞机飞行产生的涡旋流模型的紧凑模拟

Pavlo Lukianov, Lin Song
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It is about the fact that, as a second misunderstanding, an error is assumed when calculating the kinetic energy of the vortex flows: the Jacobian in cylindrical (polar) coordinates is not considered. As a result, all the mentioned models of vortex flows, which correspond to the hyperbolic law as their asymptotics in the periphery, have infinite kinetic energy. Certainly, this does not correspond to the formation and evolution of compact vortex structures. Therefore, in this work, based on overcoming the aforementioned misunderstandings, many previously obtained models of compact vortex flows, as well as those obtained for the first time, are presented. In particular, this applies to the turbulent vortex flow during the formation of a vortex sheet, which is a compact analog of the Burgers-Rott vortex - both the classical one corresponding to laminar motion and the one consisting of a laminar flow in the core and a turbulent flow on the periphery of the vortex. 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引用次数: 0

摘要

这项工作的主题是发展紧凑的涡流模拟模型,用于模拟飞机飞行和物体在流体中的运动过程中观察到的涡结构。特别强调了这一科学领域中普遍存在的两个重大误解。第一个误解是,流体包裹在一个圆圈中的静止运动被视为一个无粘的漩涡。因此,任何不明确包含粘度的涡流模型都被认为是描述无粘涡运动的模型。事实证明并非如此:流体包裹在圆形轨道上的静止粘性运动对应于一种力的自平衡——粘性力。这是第一次以明确的形式得出的结论。这是非常重要的,因为它改变了我们对力平衡的看法,即两种或两种以上不同性质的力必须存在。克服这种误解为创建现有涡旋运动模型的紧凑类似物开辟了道路。在此过程中,又消除了涡旋动力学领域的第二个普遍误解。无论我们读到哪里,我们都可以看到涡旋流的致密性与涡度场的致密性是相关联的。考虑的是涡度方程而不是速度方程,这一点很方便。因此,除了一个或两个漩涡模型,它们对应于整个空间的旋转,直到无穷大,这违反了物理学的基本定律——能量守恒和转换定律。这是关于这样一个事实,作为第二个误解,在计算涡流的动能时假设了一个错误:没有考虑柱(极)坐标中的雅可比矩阵。因此,上述所有涡旋流动模型都具有无限大的动能,其在外围的渐近解都符合双曲定律。当然,这并不符合致密涡旋结构的形成和演化。因此,在本文中,在克服上述误解的基础上,介绍了许多以前获得的紧凑涡旋流动模型,以及首次获得的模型。这尤其适用于涡旋片形成过程中的湍流涡旋流动,它是一种紧凑的burger - rott涡旋模拟——既有层流运动对应的经典涡旋,也有核心层流和涡旋外围湍流组成的涡旋。研究方法完全是理论性的。运用了理论力学、数学场论、变分法等著名定理。并将所得解与已有的非致密流的类似解进行了比较。结论。利用变分法,可以证明在不可压缩流体的边界层中形成类固体旋转运动的可能性。粘度的存在,或者更确切地说,考虑到它(边界层),表明由于开尔文-亥姆霍兹不稳定性,流动可能从平面平行运动转变为刚才提到的旋转运动。此外,本研究还获得了两个新的Burgers-Rott涡旋流动模型。第一个模型使用Burgers得到的通解,但该模型对应的是一个组合涡:虽然速度场是连续的,但涡度场具有不连续-在最大速度点。证明了这种方法是完全可能的:运动方程处处都满足,即在空间的每一点上都满足,切向应力是连续函数。由于Burgers-Rott涡旋的外围是一个不稳定的流动,提出了另一种模型-层流核心和湍流外围。当然,外围区域流体包裹的运动可以用一种速度分布来描述,而不是用Burgers的速度分布来描述。最后,考虑了使用已知的紧凑涡旋流模型来模拟von Karman涡旋街的可能性,并指出了这些模型的优点。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Compact analogs of the models of vortex flows generated by aircraft flight
The subject of this work is the development of compact analogs of vortex flows models, which are used in the modeling of vortex structures observed during the flight of an aircraft and the motion of a body in a fluid. In particular, two significant misunderstandings prevailing in this area of science are highlighted. The first misunderstanding is that the stationary motion of fluid parcels in a circle is treated as an inviscid vortex. Therefore, any vortex flow model that does not explicitly contain viscosity is considered to describe inviscid vortex motion. It has been proven that this is not so: the stationary viscous motion of fluid parcels in circular orbits corresponds to the self-balance of one force - the force of viscosity. This conclusion, in an explicit form, was made for the first time. This is very important because it changes our ideas about force balance, where two or more forces of different natures must necessarily be present. Overcoming this misunderstanding opens the way for creating compact analogs of existing models of vortex motions. Along the way, one more - the second general misunderstanding in the field of vortex dynamics was eliminated. Wherever we read it, we can see that the compactness of the vortex flow is associated with the compactness of the vorticity field. This is facilitated by the fact that the equations for vorticity and not for velocity are considered. As a result, except for one or two models of vortices, which correspond to the rotation of the entire space, up to infinity, this violates the fundamental law of physics - the law of conservation and transformation of energy. It is about the fact that, as a second misunderstanding, an error is assumed when calculating the kinetic energy of the vortex flows: the Jacobian in cylindrical (polar) coordinates is not considered. As a result, all the mentioned models of vortex flows, which correspond to the hyperbolic law as their asymptotics in the periphery, have infinite kinetic energy. Certainly, this does not correspond to the formation and evolution of compact vortex structures. Therefore, in this work, based on overcoming the aforementioned misunderstandings, many previously obtained models of compact vortex flows, as well as those obtained for the first time, are presented. In particular, this applies to the turbulent vortex flow during the formation of a vortex sheet, which is a compact analog of the Burgers-Rott vortex - both the classical one corresponding to laminar motion and the one consisting of a laminar flow in the core and a turbulent flow on the periphery of the vortex. Research methods are entirely theoretical. Well-known theorems of theoretical mechanics, mathematical theory of field, and calculus of variations, etc. are used. The obtained solutions are compared with the existing corresponding analogs of non-compact flows. Conclusions. Using the methods of calculus of variation, it was possible to show the possibility of the formation of quasi-solid-like rotational motion in a boundary layer of an incompressible fluid. The very presence of viscosity, or rather its taking into account (boundary layer), indicates a possible transition of the flow from plane-parallel motion to the just-mentioned rotational one due to the Kelvin-Helmholtz instability. In addition, two new models of the Burgers-Rott vortex flow were obtained in this study. The first model uses the general solution obtained by Burgers, but this model corresponds to a combined vortex: although the velocity field is continuous, the vorticity field has a discontinuity - at the point of maximum velocity. It is proved that such an approach is quite possible: the equation of motion is satisfied everywhere, i.e., at every point in space, and the tangential stresses are continuous functions. Since the periphery of the Burgers-Rott vortex is an unstable flow, another model is proposed - with a laminar core and a turbulent periphery. Certainly, the motion of fluid parcels in the peripheral region is described by a velocity distribution other than that of Burgers. Finally, the possible use of known models of compact vortex flows to simulate the von Karman vortex street is considered, with an indication of the advantages of these models.
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