Stator part with blade and fin arrangement in a turbomachine

A stator part for a turbomachine comprising:

• a platform defining a wall of a gas flow duct,
• a blade extending radially with respect to an axis of the turbomachine from the platform, the blade having a camber maximum, and
• a fin extending radially in the duct from a root to a tip, the root being located on the platform, the tip extending axially along the axis from a leading edge to a trailing edge, the tip having a chord length, the chord length connecting, in a straight line, the leading edge and the trailing edge,
• the fin and the blade being designed such that:
• the camber maximum is axially located between the leading edge and the trailing edge,
• a ratio of an axially measured distance between the camber maximum and the leading edge over the chord length is less than or equal to 95% and greater than or equal to 5%, and
• a fin height defined between the root and the tip varies along the axis so as to define a recess in the fin, the recess extending axially over a recess length, the recess length being less than or equal to 20% of the chord length, a projection of the camber maximum along the axis lies within a projection of the recess along the axis.