The invention relates to an
assembly (15) for an aircraft propulsion unit, comprising: - a radial bounding structure (34) for the flow of a gas flow (12b), comprising a radial
bounding surface (34a) oriented in a first direction (S1); - a first device (45a) projecting from the radial
bounding surface (34a) in the first direction (S1) and configured to have a first portion (12b1) of the gas flow pass therethrough, and wherein the first device comprises a
cowling (50) that is intended to be followed closely by the first portion (12b1) of the gas flow exiting the first device (45a), and by a second portion (12b2) of the gas flow. According to the invention, the
cowling (50) comprises a mixer (64) for mixing the second portion (12b2) with the first portion (12b1) of the gas flow.