Research Article

Propeller Modification with Groove Structure on Thrust Performance

Volume: 21 Number: 1 March 26, 2025
EN

Propeller Modification with Groove Structure on Thrust Performance

Abstract

This study includes an investigation into the application of grooves in drone propellers that inspired from the structure of a bird's wing. The designed propeller involves the application of grooves at angles of 30, 45 and 60 degrees. Main purpose of using biomimetic design is to determine whether it is effective in improving thrust performance by directing the flow to the propeller blade through the grooves. Experimental investigation of the effects of these grooves on the propeller-engine thrust and the underlying causes of these effects were tried to be presented experimentally with TiO2 based surface oil imaging technique. From the experimental results, the highest thrust value was obtained for the modified prop-60⁰ model compared to the base propeller. Thrust measurements were measured at various rmp/V values. The maximum increase in thrust improvement is reached when the engine driven by 25% nominal power.

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Ethical Statement

There are no ethical issues after the publication of this manuscript.

Thanks

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References

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  6. [6]. Kim, S. H., Chang, J. W., Sohn, M. H. 2008. Flow visualization and aerodynamic-force measurement of a dragonfly-type model. Journal of visualization; 11, 37-44.
  7. [7]. Nguyen, T. T., Byun, D. 2008. Two-dimensional aerodynamic models of insect flight for robotic flapping wing mechanisms of maximum efficiency. Journal of Bionic Engineering; 5(1), 1-11.
  8. [8]. Nelson, D., Keating, F., Leonard, J., Jacob, J. 2013. Design of a Biomimetic Unmanned Aircraft System, 51th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, Grapevine (Dallas/Ft. Worth Region), Texas, AIAA 2013-0761.

Details

Primary Language

English

Subjects

Aerospace Engineering (Other)

Journal Section

Research Article

Publication Date

March 26, 2025

Submission Date

August 9, 2024

Acceptance Date

November 25, 2024

Published in Issue

Year 2025 Volume: 21 Number: 1

APA
Özyurt, D., & Akbıyık, H. (2025). Propeller Modification with Groove Structure on Thrust Performance. Celal Bayar University Journal of Science, 21(1), 27-34. https://doi.org/10.18466/cbayarfbe.1531094
AMA
1.Özyurt D, Akbıyık H. Propeller Modification with Groove Structure on Thrust Performance. CBUJOS. 2025;21(1):27-34. doi:10.18466/cbayarfbe.1531094
Chicago
Özyurt, Duygu, and Hürrem Akbıyık. 2025. “Propeller Modification With Groove Structure on Thrust Performance”. Celal Bayar University Journal of Science 21 (1): 27-34. https://doi.org/10.18466/cbayarfbe.1531094.
EndNote
Özyurt D, Akbıyık H (March 1, 2025) Propeller Modification with Groove Structure on Thrust Performance. Celal Bayar University Journal of Science 21 1 27–34.
IEEE
[1]D. Özyurt and H. Akbıyık, “Propeller Modification with Groove Structure on Thrust Performance”, CBUJOS, vol. 21, no. 1, pp. 27–34, Mar. 2025, doi: 10.18466/cbayarfbe.1531094.
ISNAD
Özyurt, Duygu - Akbıyık, Hürrem. “Propeller Modification With Groove Structure on Thrust Performance”. Celal Bayar University Journal of Science 21/1 (March 1, 2025): 27-34. https://doi.org/10.18466/cbayarfbe.1531094.
JAMA
1.Özyurt D, Akbıyık H. Propeller Modification with Groove Structure on Thrust Performance. CBUJOS. 2025;21:27–34.
MLA
Özyurt, Duygu, and Hürrem Akbıyık. “Propeller Modification With Groove Structure on Thrust Performance”. Celal Bayar University Journal of Science, vol. 21, no. 1, Mar. 2025, pp. 27-34, doi:10.18466/cbayarfbe.1531094.
Vancouver
1.Duygu Özyurt, Hürrem Akbıyık. Propeller Modification with Groove Structure on Thrust Performance. CBUJOS. 2025 Mar. 1;21(1):27-34. doi:10.18466/cbayarfbe.1531094

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