About this document
Shuttlecock Aerodynamics: Skirt Angle Effects by 4209kirlto is a document available to read on EtoBox.
The study investigates the aerodynamic performance of a standard feathers shuttlecock using computational fluid dynamics (CFD) analysis. It finds that the drag coefficient (Cd) is influenced by the angle of skirt (Ɵ) and angle of feathers (β), with smaller Ɵ leading to lower Cd and an optimal β for maximum drag. The research suggests that Ɵ and β can be considered as design parameters to enhance shuttlecock aerodynamics.
- Author
- 4209kirlto
- Language
- EN