Process for manufacturing an assembly made of a composite material and wing and stabilizing element obtained by this process. The junction zone for a part (P) made of a composite material comprising two parts (A1, A2) in which the principal directions intersect at a non-singular angle, is made in a single operation by continuous lay-up. The 0.degree. directions of the lay-up coordinate systems (R1, R2) of the parts (A1, A2) are oriented such that these directions make an angle of close to 180.degree.-.theta..degree., where .+-..theta..degree. represents the other directions of the lay-up coordinate systems (R1, R2). Thus, the layers of fibers oriented at 0.degree. in one of the coordinate systems correspond approximately to a lay-up direction of .+-..theta..degree. in the other coordinate system.
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