4.5 Article

Drag-thrust transition and wake structures of a pitching foil undergoing asymmetric oscillation

期刊

JOURNAL OF FLUIDS AND STRUCTURES
卷 103, 期 -, 页码 -

出版社

ACADEMIC PRESS LTD- ELSEVIER SCIENCE LTD
DOI: 10.1016/j.jfluidstructs.2021.103289

关键词

Pitching foil; Asymmetric sinusoidal oscillation; Drag-thrust transition; Wake structures

资金

  1. National Natural Science Foundation of China [11672096, 91752112]
  2. Research Grant Council of Shenzhen Government, China [JCYJ20180306171921088]

向作者/读者索取更多资源

This study numerically investigates the drag-thrust transition and wake structures of a pitching foil undergoing asymmetric sinusoidal oscillation. The results show that pitching asymmetry advances the drag-thrust transition and produces P+S wake structures, affecting fluid dynamics and the formation of wake jets.
The drag-thrust transition and wake structures of a pitching foil undergoing asymmetric sinusoidal oscillation are numerically investigated for foil thickness-based Strouhal number St(D) = 0.1-0.3 and amplitude ratio A(D) = 0.5-2.0. The asymmetry in the oscillation is introduced by making one half-stroke (e.g. from the lower extreme to the upper extreme) faster than the other. The results reveal that the drag-thrust transition advances with increasing the pitching asymmetry because of enhanced thrust in the faster stroke. Similar to the reverse Karman wake generated from the symmetric oscillation, the P+S (paired and single vortices) wake identified in the case of the asymmetric oscillation can produce both drag and thrust, hence appearing around the drag-thrust transition boundary. The formation and evolution of wake structures produced by the asymmetrically oscillating foil are discussed, showing how the asymmetric oscillation affects fluid dynamics, drag-thrust transition, vortex strength, and wake jet. This work provides some new perspectives to understand the swimming and flying performance and some useful findings to design bio-inspired robots. (C) 2021 Elsevier Ltd. All rights reserved.

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