A shuttlecock including a cap and a skirt part whereto an air passage hole is formed, comprising: a rib provided to the skirt part, adjacent to a rear end of the air passage hole in a generatrix direction of the skirt part, this rib having a shape wherein air pressure difference is generated between an air flow passing through the air passage hole to flow on an inside of the rib and an air flow not passing through the air passage hole but to flow on an outside of the rib, and an aerodynamic force directed from the inside of the rib to the outside is generated and wherein a cross sectional contour of the rib has a streamline shape as the shape, the cross section achieved by cutting with a virtual plane including a central axis of the skirt part, and an outside part of the contour positioned on an outside of a virtual straight line is longer than an inside part of the contour that is positioned on the inside of the virtual straight line, the virtual straight line connecting both ends of the streamline shape in a direction along the generatrix direction and characterised in that the outside part includes two curved lines having a radius of curvatures different from each other, the radius of curvature of the curved line positioned on a front side that is closer to the cap in the generatrix direction, of the two curved lines, is smaller than the radius of curvature of the curved line positioned on a rear side further distant from the cap in the generatrix direction, a boundary between the two curved lines is positioned on the front side, of the front side and the rear side, and the inside part includes curved-line parts positioned at both ends the inside part, and a straight-line part positioned at a center thereof. a rib provided to the skirt part, adjacent to a rear end of the air passage hole in a generatrix direction of the skirt part, this rib having a shape wherein air pressure difference is generated between an air flow passing through the air passage hole to flow on an inside of the rib and an air flow not passing through the air passage hole but to flow on an outside of the rib, and an aerodynamic force directed from the inside of the rib to the outside is generated and wherein a cross sectional contour of the rib has a streamline shape as the shape, the cross section achieved by cutting with a virtual plane including a central axis of the skirt part, and an outside part of the contour positioned on an outside of a virtual straight line is longer than an inside part of the contour that is positioned on the inside of the virtual straight line, the virtual straight line connecting both ends of the streamline shape in a direction along the generatrix direction and characterised in that the outside part includes two curved lines having a radius of curvatures different from each other, the radius of curvature of the curved line positioned on a front side that is closer to the cap in the generatrix direction, of the two curved lines, is smaller than the radius of curvature of the curved line positioned on a rear side further distant from the cap in the generatrix direction, a boundary between the two curved lines is positioned on the front side, of the front side and the rear side, and the inside part includes curved-line parts positioned at both ends the inside part, and a straight-line part positioned at a center thereof.