An acoustically resistive layer for an acoustic attenuation panel (22)
forming a conduit in which there is an aerodynamic flow (18), adapted
particularly for an aircraft turbo jet engine. The panel has at least one
acoustically resistive layer (24), at least one porous structure (26) and
a reflector (28) disposed opposite the incident wave. The acoustically
resistive layer (24) is constituted by strips (30) disposed in the
direction of the flow (18), interconnected by a plurality of splints (32)
ensuring the absorption of force, particularly radially, the splints (32)
having very small surfaces ensuring the continuity of the homogeneous
character of the quantity of open surface of the acoustically resistive
layer thus formed.
