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Article

Investigating the Power Extraction of Applying Hybrid Pitching Motion on a Wing with Leading and Trailing Flaps

School of Mechanical Engineering, Kyungpook National University, Daegu 41566, Republic of Korea
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Author to whom correspondence should be addressed.
Actuators 2025, 14(2), 62; https://doi.org/10.3390/act14020062
Submission received: 6 January 2025 / Revised: 23 January 2025 / Accepted: 24 January 2025 / Published: 27 January 2025

Abstract

This research utilized a hybrid trajectory on a wing incorporating a dual flap with the goal of enhancing performance. The hybrid profiles initiate with a non-sinusoidal pattern during the interval 0.0 ≤ t/T ≤ 0.25, evolving toward a sinusoidal pattern within the range 0.25 < t/T ≤ 0.5. Similarly, the hybrid motion follows a non-sinusoidal pattern in the range 0.5 < t/T ≤ 0.75, before shifting back to a sinusoidal pattern within the range 0.75 < t/T ≤ 1.0. The effectiveness of using a hybrid trajectory on a wing with leading and trailing flaps in enhancing the energy harvesting performance is examined through numerical simulations. The results demonstrate that hybrid trajectories applied to a two-flap wing configuration outperform a single flat plate and a wing with leading and trailing flaps both operating under a sinusoidal trajectory. The wing length spans from 45% to 55%, with the leading flap length ranging from 25% to 35%. The trailing flap lengths adjust accordingly to ensure the combined total matches the flat plate’s full length, which is 100%. The wing pitch angle was fixed at 85° while the leading flap’s pitch angle varied between 40° and 55° and the pitch angle of the trailing flap ranged from 0° to 20°. The findings reveal that utilizing hybrid motion on a wing fitted with leading and trailing flaps notably improves power output in comparison to configurations with either one plate or three plates. The power output is achieved at particular dimensions: a leading flap length of 30%, a wing length of 55%, and a trailing flap length of 15%. The corresponding pitch angles are 50° for the leading flap, 85° for the wing, and 10° for the trailing flap. The aforementioned configuration results in a 34.06% increase in output power in comparison to one plate. The maximum efficiency for this setup reaches 44.21%. This underscores the superior performance of hybrid trajectories over sinusoidal trajectories in enhancing energy extraction performance.
Keywords: energy harvester; leading flaps; trailing flaps; hybrid motion; flapping flat plate energy harvester; leading flaps; trailing flaps; hybrid motion; flapping flat plate

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MDPI and ACS Style

Saleh, S.; Sohn, C.-H. Investigating the Power Extraction of Applying Hybrid Pitching Motion on a Wing with Leading and Trailing Flaps. Actuators 2025, 14, 62. https://doi.org/10.3390/act14020062

AMA Style

Saleh S, Sohn C-H. Investigating the Power Extraction of Applying Hybrid Pitching Motion on a Wing with Leading and Trailing Flaps. Actuators. 2025; 14(2):62. https://doi.org/10.3390/act14020062

Chicago/Turabian Style

Saleh, Suleiman, and Chang-Hyun Sohn. 2025. "Investigating the Power Extraction of Applying Hybrid Pitching Motion on a Wing with Leading and Trailing Flaps" Actuators 14, no. 2: 62. https://doi.org/10.3390/act14020062

APA Style

Saleh, S., & Sohn, C.-H. (2025). Investigating the Power Extraction of Applying Hybrid Pitching Motion on a Wing with Leading and Trailing Flaps. Actuators, 14(2), 62. https://doi.org/10.3390/act14020062

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