A dawn is concerned for a turbomachine. The blade (12 ') has a blade (13') and a foot (18 ') to engage in an axial groove of a disk of the turbomachine. The upstream end (450 ') of the foot is connected to a radially inner end (430') of the leading edge (431 ') of the blade by the upstream end of a connecting zone having a recess towards the downstream, so that said radially inner end of the leading edge of the blade is located further downstream than the upstream end of the foot.
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