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Review of Unsteady Vortex Flows over Slender Delta Wings

机译:细长三角翼上不稳定涡流的回顾

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摘要

A wide range of unsteady phenomena relevant to slender vortex flows over stationary and maneuvering delta wings is reviewed. The origin, characteristics, and physical mechanisms of these unsteady phenomena and their role in buffeting are discussed. Dynamic response of leading-edge vortices for maneuvering wings and mechanisms of hysteresis and time lag effects are reviewed. Issues and challenges for unsteady vortex flows over delta wings are outlined. Although the main features of the unsteady phenomena related to slender delta wings are relatively well understood, many aspects require further study. The details of the shear layer instabilities, steady and unsteady substructures, and transition need to be investigated further, Vortex wandering remains a problem in the characterization of the leading-edge vortices. Time-averaged velocity in the core of a wandering vortex is not representative of instantaneous core structure. The relationship between the shear layer instabilities and vortex wandering requires further study. The main instability associated with vortex breakdown is the helical mode instability, and the spiral form of breakdown is a consequence of this instability of the breakdown wake. The mechanisms of vortex interactions, which appear in the form of antisymmetric oscillations of breakdown locations, need to be investigated further. Whether vortex breakdown is a necessary part of these interactions is not known. Although these kinds of vortex interactions are thought to be dominant over slender wings, they also, surprisingly, exist over nonslender wings. These interactions may take very complicated forms when excited by ek-ternal disturbances. The frequency spectrum of the unsteady flow phenomena that exist over stationary wings is very wide, which is one of the challenges in numerical simulations of these flows. Vortex breakdown, vortex interactions, and vortex shedding, either alone or in combination, play an important role in wing. and fin buffeting, although vortex breakdown is the main source of buffeting over slender wings.
机译:审查了广泛的与细长涡流在固定和机动三角翼上流动有关的非稳态现象。讨论了这些不稳定现象的起源,特征和物理机制,以及它们在抖振中的作用。综述了前沿涡旋操纵机翼的动态响应以及磁滞现象和时滞效应的机理。概述了三角翼上不稳定涡流的问题和挑战。尽管与细长三角翼有关的非稳态现象的主要特征已得到相对较好的理解,但许多方面仍需要进一步研究。剪切层不稳定性,稳态和非稳态子结构以及过渡的细节有待进一步研究,涡旋漂移仍然是前沿涡旋特征化中的一个问题。徘徊涡流核心中的时间平均速度不能代表瞬时核心结构。剪切层的不稳定性和涡流之间的关系需要进一步研究。与涡旋击穿相关的主要不稳定性是螺旋模式的不稳定性,而击穿的螺旋形式是击穿尾迹的这种不稳定性的结果。以击穿位置的反对称振荡形式出现的涡旋相互作用机理,需要进一步研究。旋涡破裂是否是这些相互作用的必要部分尚不清楚。尽管这些涡旋相互作用被认为在细长的机翼上占主导地位,但令人惊讶的是,它们也存在于不细长的机翼上。当受到大脑内部干扰时,这些相互作用可能会采取非常复杂的形式。存在于固定翼上的非定常流动现象的频谱非常宽,这是对这些流动进行数值模拟的挑战之一。涡旋破裂,涡旋相互作用和涡旋脱落,无论是单独还是结合在一起,在机翼中都起着重要作用。和鳍式抖振,尽管旋涡破裂是细长机翼上抖振的主要来源。

著录项

  • 来源
    《Journal of Aircraft》 |2005年第2期|p.299-319|共21页
  • 作者

    Ismet Gursul;

  • 作者单位

    University of Bath, Bath, England BA2 7AY, United Kingdom;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 航空;
  • 关键词

  • 入库时间 2022-08-18 02:33:57

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