振荡翼升力产生、尾流拓扑和运动学的关联

IF 1.5 4区 工程技术 Q2 ENGINEERING, AEROSPACE
Suyash Verma, M. Khalid, A. Hemmati
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引用次数: 4

摘要

在蓝减频率(0.16≤f *≤0.48)、相位偏移(0°≤φ≤315°)和雷诺数(1000≤Re≤4000)范围内,对振荡箔后的升力产生和尾迹拓扑演变与起伏和俯俯向联合运动之间的关联进行了数值研究。俯距主导的运动学与φ≤120°和φ≥225°的范围一致,表明前缘涡被抑制,而后缘涡主导尾流,且频率越来越低。这对应于尾流拓扑从2p到反向Von Kármán尾流模式的过渡。相反,升沉主导的运动(120°< φ≤225°)没有随着f *的增加而表现出任何尾流拓扑转换。与升力主导相关的时间升力变化进一步揭示了在振荡周期内达到峰值升力产生所需时间的对称特征。然而,随着运动学从垂向俯仰主导转变,这种时间对称性丢失了。分析了振荡周期四分之一阶段的尾迹演化和升力特征,揭示了在升沉和俯仰主导的运动过程中,这两个过程之间存在对应关系。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
On association of lift generation, wake topology and kinematics of oscillating foils
The association of lift generation and evolution of wake topology behind an oscillating foil with combined heaving and pitching motion is investigated numerically at a range of bluereduced frequency (0.16 ≤ f * ≤ 0.48), phase offset (0 ∘ ≤ ϕ ≤ 315 ∘ ) and Reynolds number (1000 ≤ R e ≤ 4000). The pitch-dominated kinematics that coincide with the range of ϕ ≤ 120 ∘ and ϕ ≥ 225 ∘ suggests that leading edge vortices are suppressed while trailing edge vortices dominate the wake with increasing reduced frequency. This corresponds to a transition in wake topology from a 2 P to a reverse Von Kármán wake mode. Contrarily, heave dominated kinematics (120 ∘ < ϕ ≤ 225 ∘ ) did not exhibit any wake topology transition with increasing f * . The temporal lift variation associated with heave-dominated regime further revealed a symmetric feature in terms of the time taken to attain peak lift generation within an oscillation cycle. This temporal symmetry was, however, lost as kinematics transitioned from heave- to pitch-dominated regime. Analyzing the wake evolution and lift features at quarter phase of an oscillation cycle revealed the existence of a correspondence between the two processes during the heave- and pitch-dominated kinematics.
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来源期刊
CiteScore
3.00
自引率
7.10%
发文量
13
审稿时长
>12 weeks
期刊介绍: The role of the International Journal of Micro Air Vehicles is to provide the scientific and engineering community with a peer-reviewed open access journal dedicated to publishing high-quality technical articles summarizing both fundamental and applied research in the area of micro air vehicles.
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