Effect of Hopf-Hopf bifurcation on the post-flutter behavior of a three-degree-of-freedom airfoil

IF 5 1区 工程技术 Q1 ENGINEERING, AEROSPACE Aerospace Science and Technology Pub Date : 2024-08-27 DOI:10.1016/j.ast.2024.109525
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Abstract

The post-flutter dynamics of a three-degree-of-freedom nonlinear airfoil with unsteady aerodynamics are investigated based on the Hopf-Hopf bifurcation theory. Many prior works have relied on Hopf bifurcation theory to predict flutter behavior in airfoil systems. Although this approach facilitates flutter prediction and characterization of post-flutter behavior in numerous scenarios, it may be invalid in specific instances, such as when the Hopf bifurcation of the system degenerates. Therefore, this study focuses on a classical degenerate case of Hopf bifurcation in airfoil systems, specifically the Hopf-Hopf bifurcation. We show that the system undergoes various Hopf-Hopf bifurcations under specific parameter conditions as the center of gravity shifts. The local dynamics near the Hopf-Hopf bifurcation points are represented, including quasiperiodic oscillations on a three-dimensional torus. The airfoil begins to oscillate quasiperiodically after the airflow speed crosses specific Hopf-Hopf bifurcation points. The study also uncovers complex quasiperiodic crises and quasiperiodic hysteresis loops, which have not been reported in previous studies of aeroelastic systems. Then, many singularities and bifurcation curves are obtained near the Hopf-Hopf bifurcation point by semiglobal unfolding. Furthermore, the influence of stall effects on the bifurcation structure of the system is represented. It is shown that the types of Hopf-Hopf bifurcations may vary with the changes of stall effects, influencing the system's semiglobal bifurcation structures consequently. For all Hopf-Hopf bifurcation scenarios, stall effects affect one of the Neimark-Sacker bifurcation curve structures unfolded from the Hopf-Hopf bifurcation point significantly, while the other Neimark-Sacker bifurcation curve experiences minimal impact from stall effects. Moreover, a large nonlinear stall coefficient will postpone the onset of quasiperiodic/chaotic oscillations.

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霍普夫-霍普夫分岔对三自由度机翼扑翼后行为的影响
基于霍普夫-霍普夫分岔理论,研究了具有非稳态空气动力学的三自由度非线性机翼的扑翼后动力学。之前的许多研究都依赖霍普夫分岔理论来预测机翼系统的扑翼行为。虽然这种方法有助于在许多情况下预测扑翼和描述扑翼后的行为,但在特定情况下可能无效,例如当系统的霍普夫分岔退化时。因此,本研究侧重于机翼系统中霍普夫分岔的经典退化情况,特别是霍普夫-霍普夫分岔。我们的研究表明,在特定参数条件下,随着重心的移动,系统会发生各种霍普夫-霍普夫分岔。我们展示了霍普夫-霍普夫分岔点附近的局部动力学,包括三维环上的准周期振荡。气流速度越过特定的霍普夫-霍普夫分岔点后,机翼开始出现准周期振荡。研究还发现了复杂的准周期危机和准周期滞后环,这在以往的气动弹性系统研究中从未报道过。然后,通过半全局展开,在霍普夫-霍普夫分岔点附近获得了许多奇点和分岔曲线。此外,还体现了失速效应对系统分岔结构的影响。结果表明,Hopf-Hopf 分岔的类型会随着失速效应的变化而变化,从而影响系统的半全局分岔结构。在所有霍普夫-霍普夫分岔情况下,失速效应对从霍普夫-霍普夫分岔点展开的一条 Neimark-Sacker 分岔曲线结构影响很大,而另一条 Neimark-Sacker 分岔曲线受失速效应的影响很小。此外,较大的非线性失速系数会推迟准周期/混乱振荡的发生。
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来源期刊
Aerospace Science and Technology
Aerospace Science and Technology 工程技术-工程:宇航
CiteScore
10.30
自引率
28.60%
发文量
654
审稿时长
54 days
期刊介绍: Aerospace Science and Technology publishes articles of outstanding scientific quality. Each article is reviewed by two referees. The journal welcomes papers from a wide range of countries. This journal publishes original papers, review articles and short communications related to all fields of aerospace research, fundamental and applied, potential applications of which are clearly related to: • The design and the manufacture of aircraft, helicopters, missiles, launchers and satellites • The control of their environment • The study of various systems they are involved in, as supports or as targets. Authors are invited to submit papers on new advances in the following topics to aerospace applications: • Fluid dynamics • Energetics and propulsion • Materials and structures • Flight mechanics • Navigation, guidance and control • Acoustics • Optics • Electromagnetism and radar • Signal and image processing • Information processing • Data fusion • Decision aid • Human behaviour • Robotics and intelligent systems • Complex system engineering. Etc.
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