Abstract: The invention relates to the field of compressors, and specifically a compressor stage (100) comprising at least a casing (101) delimiting an air passage (2), a stator (102) comprising a plurality of guide vanes (103) arranged radially around a central axis (X) in the air passage (2), and a rotor (104) suitable for rotating about the central axis (X) relative to the stator (102) and comprising a plurality of blades (105) arranged radially around the central axis (X) in the air passage (2) downstream from the guide vanes (103). Each blade (105) of the rotor (104) extends from a blade root (105a) to a blade tip (105b) further away from the central axis (X) than the blade root (105a) and presents radial clearance (j) between the blade tip (105b) and the casing (101).