下落飞行器的稳定性

IF 3.4 2区 工程技术 Q1 ENGINEERING, MECHANICAL
Sung-Ik Sohn
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We consider four folding angles of the wings: <span><math><mrow><msub><mrow><mi>ϕ</mi></mrow><mrow><mn>0</mn></mrow></msub><mo>=</mo><mn>1</mn><msup><mrow><mn>0</mn></mrow><mrow><mo>∘</mo></mrow></msup><mo>,</mo><mn>2</mn><msup><mrow><mn>0</mn></mrow><mrow><mo>∘</mo></mrow></msup><mo>,</mo><mn>3</mn><msup><mrow><mn>0</mn></mrow><mrow><mo>∘</mo></mrow></msup></mrow></math></span>, and 45°, with the Froude number <span><math><mrow><mtext>Fr</mtext><mo>=</mo><mn>1</mn></mrow></math></span>. Our results show significant differences in the stability of flyers for varying the folding angle. For <span><math><mrow><msub><mrow><mi>ϕ</mi></mrow><mrow><mn>0</mn></mrow></msub><mo>=</mo><mn>1</mn><msup><mrow><mn>0</mn></mrow><mrow><mo>∘</mo></mrow></msup></mrow></math></span>, the oscillation of the side-to-side motion increases rapidly, whereas for <span><math><mrow><msub><mrow><mi>ϕ</mi></mrow><mrow><mn>0</mn></mrow></msub><mo>=</mo><mn>2</mn><msup><mrow><mn>0</mn></mrow><mrow><mo>∘</mo></mrow></msup></mrow></math></span> and 30°, the flyers fall similarly and the oscillation increases much more slowly than in the case of <span><math><mrow><msub><mrow><mi>ϕ</mi></mrow><mrow><mn>0</mn></mrow></msub><mo>=</mo><mn>1</mn><msup><mrow><mn>0</mn></mrow><mrow><mo>∘</mo></mrow></msup></mrow></math></span>. For <span><math><mrow><msub><mrow><mi>ϕ</mi></mrow><mrow><mn>0</mn></mrow></msub><mo>=</mo><mn>4</mn><msup><mrow><mn>5</mn></mrow><mrow><mo>∘</mo></mrow></msup></mrow></math></span>, the flyer falls stably at early times, but the oscillation later grows rapidly. We also examine the effects of varying the Froude number and the center of mass of the body, with a fixed angle of <span><math><mrow><msub><mrow><mi>ϕ</mi></mrow><mrow><mn>0</mn></mrow></msub><mo>=</mo><mn>2</mn><msup><mrow><mn>0</mn></mrow><mrow><mo>∘</mo></mrow></msup></mrow></math></span>. The flyer maintains a side-to-side oscillation for <span><math><mrow><mtext>Fr</mtext><mo>=</mo><mn>0</mn><mo>.</mo><mn>5</mn></mrow></math></span>, whereas it becomes unstable and eventually flips for <span><math><mrow><mtext>Fr</mtext><mo>=</mo><mn>2</mn></mrow></math></span>. It is found that lowering the center of mass stabilizes the flyer, whereas heightening the center of mass destabilizes it. The results on the flyer’s stability have practical implications in real-world applications such as air-gliders and bio-inspired flyers.</div></div>","PeriodicalId":54834,"journal":{"name":"Journal of Fluids and Structures","volume":"137 ","pages":"Article 104336"},"PeriodicalIF":3.4000,"publicationDate":"2025-05-28","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Stability of falling flyers\",\"authors\":\"Sung-Ik Sohn\",\"doi\":\"10.1016/j.jfluidstructs.2025.104336\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"<div><div>The motion of falling <span><math><mo>∨</mo></math></span>-flyers is studied using an inviscid vortex shedding model. The body and vortices separated from the edge of the body are described by vortex sheets. The model provides a highly resolved vorticity field of the flow. We investigate the stability of falling flyers for various physical parameters. At high Reynolds numbers, the dynamics of falling bodies are characterized by the Froude number, which represents the relative importance of body inertia. We consider four folding angles of the wings: <span><math><mrow><msub><mrow><mi>ϕ</mi></mrow><mrow><mn>0</mn></mrow></msub><mo>=</mo><mn>1</mn><msup><mrow><mn>0</mn></mrow><mrow><mo>∘</mo></mrow></msup><mo>,</mo><mn>2</mn><msup><mrow><mn>0</mn></mrow><mrow><mo>∘</mo></mrow></msup><mo>,</mo><mn>3</mn><msup><mrow><mn>0</mn></mrow><mrow><mo>∘</mo></mrow></msup></mrow></math></span>, and 45°, with the Froude number <span><math><mrow><mtext>Fr</mtext><mo>=</mo><mn>1</mn></mrow></math></span>. Our results show significant differences in the stability of flyers for varying the folding angle. For <span><math><mrow><msub><mrow><mi>ϕ</mi></mrow><mrow><mn>0</mn></mrow></msub><mo>=</mo><mn>1</mn><msup><mrow><mn>0</mn></mrow><mrow><mo>∘</mo></mrow></msup></mrow></math></span>, the oscillation of the side-to-side motion increases rapidly, whereas for <span><math><mrow><msub><mrow><mi>ϕ</mi></mrow><mrow><mn>0</mn></mrow></msub><mo>=</mo><mn>2</mn><msup><mrow><mn>0</mn></mrow><mrow><mo>∘</mo></mrow></msup></mrow></math></span> and 30°, the flyers fall similarly and the oscillation increases much more slowly than in the case of <span><math><mrow><msub><mrow><mi>ϕ</mi></mrow><mrow><mn>0</mn></mrow></msub><mo>=</mo><mn>1</mn><msup><mrow><mn>0</mn></mrow><mrow><mo>∘</mo></mrow></msup></mrow></math></span>. For <span><math><mrow><msub><mrow><mi>ϕ</mi></mrow><mrow><mn>0</mn></mrow></msub><mo>=</mo><mn>4</mn><msup><mrow><mn>5</mn></mrow><mrow><mo>∘</mo></mrow></msup></mrow></math></span>, the flyer falls stably at early times, but the oscillation later grows rapidly. We also examine the effects of varying the Froude number and the center of mass of the body, with a fixed angle of <span><math><mrow><msub><mrow><mi>ϕ</mi></mrow><mrow><mn>0</mn></mrow></msub><mo>=</mo><mn>2</mn><msup><mrow><mn>0</mn></mrow><mrow><mo>∘</mo></mrow></msup></mrow></math></span>. The flyer maintains a side-to-side oscillation for <span><math><mrow><mtext>Fr</mtext><mo>=</mo><mn>0</mn><mo>.</mo><mn>5</mn></mrow></math></span>, whereas it becomes unstable and eventually flips for <span><math><mrow><mtext>Fr</mtext><mo>=</mo><mn>2</mn></mrow></math></span>. It is found that lowering the center of mass stabilizes the flyer, whereas heightening the center of mass destabilizes it. 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引用次数: 0

摘要

用无粘涡脱落模型研究了落片的运动。漩涡体和从漩涡体边缘分离出来的漩涡用漩涡片来描述。该模型提供了一个高度分辨的气流涡度场。我们研究了不同物理参数下飞片的稳定性。在高雷诺数下,落体动力学的特征是弗劳德数,它代表了物体惯性的相对重要性。我们考虑翅膀的四种折叠角度:ϕ0=10°、20°、30°和45°,弗劳德数Fr=1。我们的研究结果表明,不同的折叠角度对传单的稳定性有显著的影响。对于ϕ0=10°,两侧运动的振荡迅速增加,而对于ϕ0=20°和30°,飞人的下落相似,而且振荡的增加速度比ϕ0=10°要慢得多。对于ϕ0=45°,飞行体在早期稳定下降,但后来的振荡迅速增加。我们还研究了改变弗劳德数和身体质心的影响,并以一个固定的角(ϕ0=20°)来衡量。当Fr=0.5时,飞片保持左右振荡,而当Fr=2时,飞片变得不稳定并最终翻转。研究发现,降低质心使飞片稳定,而提高质心使飞片失稳。对飞行器稳定性的研究结果在诸如空气滑翔机和仿生飞行器等实际应用中具有实际意义。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Stability of falling flyers
The motion of falling -flyers is studied using an inviscid vortex shedding model. The body and vortices separated from the edge of the body are described by vortex sheets. The model provides a highly resolved vorticity field of the flow. We investigate the stability of falling flyers for various physical parameters. At high Reynolds numbers, the dynamics of falling bodies are characterized by the Froude number, which represents the relative importance of body inertia. We consider four folding angles of the wings: ϕ0=10,20,30, and 45°, with the Froude number Fr=1. Our results show significant differences in the stability of flyers for varying the folding angle. For ϕ0=10, the oscillation of the side-to-side motion increases rapidly, whereas for ϕ0=20 and 30°, the flyers fall similarly and the oscillation increases much more slowly than in the case of ϕ0=10. For ϕ0=45, the flyer falls stably at early times, but the oscillation later grows rapidly. We also examine the effects of varying the Froude number and the center of mass of the body, with a fixed angle of ϕ0=20. The flyer maintains a side-to-side oscillation for Fr=0.5, whereas it becomes unstable and eventually flips for Fr=2. It is found that lowering the center of mass stabilizes the flyer, whereas heightening the center of mass destabilizes it. The results on the flyer’s stability have practical implications in real-world applications such as air-gliders and bio-inspired flyers.
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来源期刊
Journal of Fluids and Structures
Journal of Fluids and Structures 工程技术-工程:机械
CiteScore
6.90
自引率
8.30%
发文量
173
审稿时长
65 days
期刊介绍: The Journal of Fluids and Structures serves as a focal point and a forum for the exchange of ideas, for the many kinds of specialists and practitioners concerned with fluid–structure interactions and the dynamics of systems related thereto, in any field. One of its aims is to foster the cross–fertilization of ideas, methods and techniques in the various disciplines involved. The journal publishes papers that present original and significant contributions on all aspects of the mechanical interactions between fluids and solids, regardless of scale.
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