The invention relates to a blade
cascade for a flow engine, especially a
steam turbine, comprising a plurality of profiled blades, especially profiled rotor blades (1), having an intake side (SS), a pressure side (DS), a median line (Sk) and a chord length (s) between a blade
leading edge and a blade
trailing edge. The invention is characterized in that a quotient of the chord length (s) for a maximum height (fSS) of the intake side (SS) is between 0.53 and 0.55, a maximum height (fDS) of the pressure side (DS) is between 0.19 and 0.21, a maximum height (fSk) of the median line (Sk) is between 0.36 and 0.38, a
diameter (Dmax / s) of a maximum circle extending between the intake and the pressure side is between 0.34 and 0.36, its distance between centers (xDmax / s) is between 0.37 and 0.39, its height in the center (fxDmax / s) is between 0.35 and 0.37, a
diameter (De / s) of its
leading edge circle (3) is between 0.025 and 0.045, a
diameter (Da / s) of a
trailing edge circle (4) is between 0.01 and 0.02, a
radius of curvature of the intake side (SS) at a distance (XRkSS0.1) of 0.1 times the chord length (s) is between 0.39 and 0.41, a
radius of curvature of the intake side (SS) at a distance (XRkSS0.75) of 0.75 times the chord length (s) is between 0.83 and 0.85, a
radius of curvature of the pressure side (DS) at a distance (XRKD0.15) of 0.15 times the chord length (s) is between 0.74 and 0.76, and / or a
radius of curvature of the pressure side (DS) at a distance (XRkDS0.80) of 0.80 times the chord length (s) is between 0.55 and 0.57.