{"title":"扑动旗子的全局模态分析","authors":"Andres Goza, T. Colonius","doi":"10.1615/tsfp10.190","DOIUrl":null,"url":null,"abstract":"We perform a global stability analysis of a flapping flag in the conventional configuration, in which the flag is pinned or clamped at its leading edge, and in the inverted configuration, in which the flag is clamped at its trailing edge. Specifically, we consider fully coupled fluid-structure interaction for two-dimensional flags at low Reynolds numbers. For the conventional configuration, we show that the unstable global modes accurately predict the onset of flapping for a wide range of mass and stiffness ratios. For the inverted configuration, we identify a stable deformed equilibrium state and demonstrate that as the flag becomes less stiff, this equilibrium undergoes a supercritical Hopf bifurcation in which the least damped mode transitions to instability. Previous stability analyses of inverted flags computed the leading mode of the undeformed equilibrium state and found it to be a zero-frequency (non-flapping) mode, which does not reflect the inherent flapping behavior. We show that the leading mode of the deformed equilibrium is associated with a non-zero frequency, and therefore offers a mechanism for flapping. We emphasize that for both configurations the global modes are obtained from the fully-coupled flow-flag system, and therefore reveal both the most dominant flag shapes and the corresponding flow structures that are pivotal to flag flapping behavior. INTRODUCTION Global stability analysis has been used to elucidate important instability-driving mechanisms in a variety of fluid flows, including bluff body flows (Noack & Eckelmann, 1994), jet flows (Bagheri et al., 2009), and boundary layers (Ehrenstein & Gallaire, 2005). Extending this analysis to fully-coupled flow-structure interaction problems with deforming bodies presents several challenges, and (to our knowledge) has not been done before. We present here an analysis of the fully-coupled problem of flow past a deformable flag in both the conventional and inverted configurations, as depicted in figure 1.","PeriodicalId":266791,"journal":{"name":"Proceeding of Tenth International Symposium on Turbulence and Shear Flow Phenomena","volume":"110 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"1900-01-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"4","resultStr":"{\"title\":\"A GLOBAL MODE ANALYSIS OF FLAPPING FLAGS\",\"authors\":\"Andres Goza, T. 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Previous stability analyses of inverted flags computed the leading mode of the undeformed equilibrium state and found it to be a zero-frequency (non-flapping) mode, which does not reflect the inherent flapping behavior. We show that the leading mode of the deformed equilibrium is associated with a non-zero frequency, and therefore offers a mechanism for flapping. We emphasize that for both configurations the global modes are obtained from the fully-coupled flow-flag system, and therefore reveal both the most dominant flag shapes and the corresponding flow structures that are pivotal to flag flapping behavior. INTRODUCTION Global stability analysis has been used to elucidate important instability-driving mechanisms in a variety of fluid flows, including bluff body flows (Noack & Eckelmann, 1994), jet flows (Bagheri et al., 2009), and boundary layers (Ehrenstein & Gallaire, 2005). Extending this analysis to fully-coupled flow-structure interaction problems with deforming bodies presents several challenges, and (to our knowledge) has not been done before. We present here an analysis of the fully-coupled problem of flow past a deformable flag in both the conventional and inverted configurations, as depicted in figure 1.\",\"PeriodicalId\":266791,\"journal\":{\"name\":\"Proceeding of Tenth International Symposium on Turbulence and Shear Flow Phenomena\",\"volume\":\"110 1\",\"pages\":\"0\"},\"PeriodicalIF\":0.0000,\"publicationDate\":\"1900-01-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"4\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Proceeding of Tenth International Symposium on Turbulence and Shear Flow Phenomena\",\"FirstCategoryId\":\"1085\",\"ListUrlMain\":\"https://doi.org/10.1615/tsfp10.190\",\"RegionNum\":0,\"RegionCategory\":null,\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"\",\"JCRName\":\"\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Proceeding of Tenth International Symposium on Turbulence and Shear Flow Phenomena","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1615/tsfp10.190","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 4
摘要
我们执行一个整体的稳定性分析,在传统的配置,其中的旗帜被固定或夹在其前缘,在倒立的配置,其中的旗帜被夹在其后缘。具体地说,我们考虑了低雷诺数下二维标志的完全耦合流固相互作用。对于传统结构,我们证明了不稳定全局模态准确地预测了大范围质量和刚度比下扑动的开始。对于倒构型,我们确定了一个稳定的变形平衡状态,并证明当标志变得不那么僵硬时,这个平衡经历了一个超临界Hopf分岔,其中最小阻尼模式转变为不稳定。以往的倒旗稳定性分析计算了未变形平衡态的先导模态,发现其为零频率(非扑动)模态,不能反映固有的扑动行为。我们证明了变形平衡的先导模态与非零频率相关,因此提供了一种扑动机制。我们强调,对于这两种构型,全局模态都是从完全耦合的流旗系统中获得的,因此揭示了最主要的旗形和对旗扑动行为至关重要的相应流结构。全球稳定性分析已被用于阐明各种流体流动中重要的不稳定性驱动机制,包括钝体流动(Noack & Eckelmann, 1994)、射流(Bagheri et al., 2009)和边界层(Ehrenstein & Gallaire, 2005)。将这种分析扩展到具有变形体的完全耦合流-结构相互作用问题提出了几个挑战,并且(据我们所知)以前没有做过。如图1所示,我们在这里分析了在常规配置和反转配置中流过可变形标志的全耦合问题。
We perform a global stability analysis of a flapping flag in the conventional configuration, in which the flag is pinned or clamped at its leading edge, and in the inverted configuration, in which the flag is clamped at its trailing edge. Specifically, we consider fully coupled fluid-structure interaction for two-dimensional flags at low Reynolds numbers. For the conventional configuration, we show that the unstable global modes accurately predict the onset of flapping for a wide range of mass and stiffness ratios. For the inverted configuration, we identify a stable deformed equilibrium state and demonstrate that as the flag becomes less stiff, this equilibrium undergoes a supercritical Hopf bifurcation in which the least damped mode transitions to instability. Previous stability analyses of inverted flags computed the leading mode of the undeformed equilibrium state and found it to be a zero-frequency (non-flapping) mode, which does not reflect the inherent flapping behavior. We show that the leading mode of the deformed equilibrium is associated with a non-zero frequency, and therefore offers a mechanism for flapping. We emphasize that for both configurations the global modes are obtained from the fully-coupled flow-flag system, and therefore reveal both the most dominant flag shapes and the corresponding flow structures that are pivotal to flag flapping behavior. INTRODUCTION Global stability analysis has been used to elucidate important instability-driving mechanisms in a variety of fluid flows, including bluff body flows (Noack & Eckelmann, 1994), jet flows (Bagheri et al., 2009), and boundary layers (Ehrenstein & Gallaire, 2005). Extending this analysis to fully-coupled flow-structure interaction problems with deforming bodies presents several challenges, and (to our knowledge) has not been done before. We present here an analysis of the fully-coupled problem of flow past a deformable flag in both the conventional and inverted configurations, as depicted in figure 1.