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Stream/Area:
-
Subject:
-
Paper ID:
IJSREM68339
Volume:
10 |
10 |
Oct 2026
Pages:
1-10
Publication Frequency:
Monthly (12 issues per year)
License:International Journal of Scientific Research in Engineering and Management follows the Creative Commons Attribution 4.0 (CC BY 4.0) License, allowing free use and distribution with proper attribution.

Department of Mechanical Engineering
Priyadarshini College of Engineering, Nagpur

Department of Mechanical Engineering
Priyadarshini College of Engineering, Nagpur

Department of Mechanical Engineering
Priyadarshini College of Engineering, Nagpur

Department of Mechanical Engineering
Priyadarshini College of Engineering, Nagpur

Department of Mechanical Engineering
Priyadarshini College of Engineering, Nagpur

Department of Mechanical Engineering
Priyadarshini College of Engineering, Nagpur

Department of Mechanical Engineering
Priyadarshini College of Engineering, Nagpur
This study explores ceiling fan performance based on blade geometry, spinning speed, and the effect of the blade surface interacting with the airflow. In particular, this study describes the design-based assessment of Dimple Wing, which represents a surface modification that can be attached to compatible ceiling fan blades. The study analyzes CAD models and other materials describing the design of the proposed surface modification in order to establish a basis for future performance assessment of the Dimple Wing surface modification. The reference configuration described in the project involves three-blade ceiling fan having diameter equal to 1200 mm. An inspection of the available mesh produces a geometric characterization of the Dimple Wing attachment part. However, more details such as physical scale, exact parameters of the dimples, and their exact placement must be verified. Possible aerodynamic consequences of the Dimple Wing attachment are discussed, in particular with regard to boundary layer dynamics, flow separation, and pressure drag. However, in the absence of validated CFD modeling results and relevant experiments, this study makes no claim about any positive changes in the efficiency, power consumption, airflow or noise reduction. Comparison with an unmodified configuration may be used as a subject of future research.
KEYWORDS
In this study, a preliminary design of Dimple Wing is presented along with a brief geometric evaluation of the attachment as a dimpled-surface modification suitable for conventional ceiling-fan blades. In this analysis, the focus is placed on describing the design, evaluating the CAD and STL files, analyzing the physical prototype, and exploring the possible aerodynamic consequences associated with installation of a dimpled-surface on a rotating fan blade. The preliminary evaluation sets the ground for further research as it is focused on design-related issues. Nonetheless, it should be noted that there are some uncertainties concerning scale and dimensions of the geometry, as well as details of the attachment and material. These aspects play an important role in determining whether the design is suitable for installation on a ceiling fan blade. It has been shown that dimpled surfaces may affect the flow properties under certain conditions. Nonetheless, since the effects associated with the dimpled surfaces depend on geometry, flow regime, and operating parameters, results of studies on dimpled surfaces cannot be taken as an evidence of improved performance of ceiling fans. Unfortunately, no validated CFD simulations and no experimental measurements have been conducted. As a result, the effect of Dimple Wing on airflow delivery, electric power consumption, rotational speed, noise, and efficiency remains unknown.
[1] E. Adeeb, A. Maqsood, A. Mushtaq, and C. H. Sohn, “Parametric study and optimization of ceiling fan blades for improved aerodynamic performance,” Journal of Applied Fluid Mechanics, vol. 9, no. 6, pp. 2905–2916, 2016. [2] W. Chen et al., “Experimental and numerical investigations of indoor air movement distribution with an office ceiling fan,” Building and Environment, vol. 130, pp. 14–26, 2018. [3] F. Gattere, A. Chiarini, and M. Quadrio, “Dimples for skin-friction drag reduction: Status and perspectives,” Fluids, vol. 7, no. 7, Art. no. 240, 2022. [4] M. van Nesselrooij et al., “Drag reduction by means of dimpled surfaces in turbulent boundary layers,” Experiments in Fluids, vol. 57, Art. no. 142, 2016. [5] O. W. G. van Campenhout et al., “Experimental and numerical investigation into the drag performance of dimpled surfaces in a turbulent boundary layer,” International Journal of Heat and Fluid Flow, vol. 100, Art. no. 109110, 2023. [6] Y. K. İlter et al., “An experimental investigation into the drag reduction performance of dimpled plates in a fully turbulent channel flow,” Ocean Engineering, vol. 307, Art. no. 118198, 2024.
Publication Date
10/26/2026
Peer Review Type
Double-Blind Peer Review
Review Rounds: 2
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Conflict of Interest
The authors declare no conflict of interest related to this research work.
Funding Information
No funding information available for this research.
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