2021
DOI: 10.1063/5.0063992
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Flow map of foil undergoing combined fast and slow pitching

Abstract: The drag-thrust transition and wake structures of a pitching foil undergoing combinations of fast and slow pitching are systematically investigated. The foil locomotion having combinations of fast and slow pitching is made by setting a variable s defined as the fraction of the pitching time required on the upper side of the wake centerline. On the other hand, time 1-s is required for the foil to pitch on the lower side of the wake centerline. Compared to the symmetric pitching (s = 0.5) case, the time-mean thr… Show more

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Cited by 10 publications
(9 citation statements)
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“…2019; Chao et al. 2021 b ). The emergence of the 2S aligned wake at the KV–RKV boundary (red dashed line) precedes the drag–thrust boundary (black solid line) in the St -- Re map (figure 17).…”
Section: Resultsmentioning
confidence: 99%
See 2 more Smart Citations
“…2019; Chao et al. 2021 b ). The emergence of the 2S aligned wake at the KV–RKV boundary (red dashed line) precedes the drag–thrust boundary (black solid line) in the St -- Re map (figure 17).…”
Section: Resultsmentioning
confidence: 99%
“…2019; Chao, Alam & Ji 2021 a ; Chao et al. 2021 b ). Alam & Muhammad (2020) analysed the fluid dynamics based on inertia, using relative angular acceleration with respect to the foil, showing that the fluid dynamics is strongly dictated by the inertia of the foil.…”
Section: Introductionmentioning
confidence: 99%
See 1 more Smart Citation
“…The influence of pitch and heave amplitude on propulsion has not been comprehensively investigated for tandem flapping foils. However, some of the works [38][39][40][41][42][43] deal with the effect of these parameters on a single foil. The St -pitch amplitude parametric space was studied for a single foil and a rich spectrum of wake behavior was observed 40,41 .…”
Section: Introductionmentioning
confidence: 99%
“…However, some of the works [38][39][40][41][42][43] deal with the effect of these parameters on a single foil. The St -pitch amplitude parametric space was studied for a single foil and a rich spectrum of wake behavior was observed 40,41 . In the case of asymmetric foil motion 42 , the mean thrust coefficient was noted to increase with pitch amplitude at Re = 3000 and Re = 10000.…”
Section: Introductionmentioning
confidence: 99%