Surface flow modification of aerofoils for automotive racing car applications

Allarton, Richard; Yao, Jun; Clifford, Tyler; Hitchborn, Benjamin; Parker, Liam J; Shaw, Joshua

Abstract

An aerofoil commonly used in aerospace engineering to produce lift is also employed in the motor sport industry to produce downforce for improving traction during cornering. This paper investigates aerofoil surface modification through 'golf ball dimpling', used to reduce flow separation behind a golf ball. The studies of other researchers have shown that this type of design can have a positive effect on improving aerofoil performance. However, no optimization information of dimple sizing is given in literature. Therefore, three types of dimpling sized at 5, 10 and 15 mm are applied to the surface of a NACA 6615 wing at 25% chord length from the leading edge in this study using Computational Fluid Dynamics (CFD) as an initial design process. Then a physical model, made through 3D printing additive manufacturing (AM), is tested at angles of attack (AoA) ranging from 0 to 20 and wind speed up to 30 m/s in a subsonic wind tunnel. Experimental and CFD results show that the smallest dimple size provides the most significant increase on lift to drag ratio at high AoA above 10. This ratio increases further with the wind speed, indicating that a high AoA wing favors down force to improve drag reduction performance.

• Journal Article Type: Article
• Acceptance Date: Dec 1, 2019
• Online Publication Date: Apr 20, 2020
• Publication Date: Jun 30, 2020
• Deposit Date: Apr 17, 2021
• Journal: International Journal of Modern Physics B
• Print ISSN: 0217-9792
• Electronic ISSN: 1793-6578
• Publisher: World Scientific Publishing
• Peer Reviewed: Peer Reviewed
• Volume: 34
• Issue: 14n16
• Article Number: 2040096
• DOI: https://doi.org/10.1142/s0217979220400962
• Keywords: Statistical and Nonlinear Physics; Condensed Matter Physics
• Public URL: https://uwe-repository.worktribe.com/output/7263348