Combustor with resonator for gas turbine engine

A method for assembling a combustor, the method comprising:

• forming a resonator segment comprising a plurality of resonator necks, each resonator neck of the plurality of resonator necks comprising a resonator inlet and a resonator outlet, each resonator neck defining a nonlinear flow path between the resonator inlet and the resonator outlet;
• directly attaching the resonator segment on a wall of the combustor, the wall defining a combustor interior to receive a fluid, the wall having a slot extending through the wall, the resonator segment directly attached to the wall to discharge the fluid from the resonator outlet directly into the combustor interior through the slot;
• and
• connecting a resonator box to the wall, the resonator segment disposed within the resonator box, the resonator segment and the resonator box cooperating defining a resonator,
• wherein the resonator neck comprises a first portion extending from the resonator inlet to a turning point and a second portion extending from the turning point to the resonator outlet, and wherein the resonator segment is formed such that the first portion and the second portion cooperate to define an angle that is between 15 degrees to 165 degrees.