Fuel nozzle for a gas turbomachine

A fuel nozzle for a gas turbomachine comprising:

• an outer nozzle body including an inner surface defining a mixing zone;
• an inner nozzle body arranged within the outer nozzle body and extending along the mixing zone, the inner nozzle body including a fluid passage;
• at least one flow affector extending from the inner nozzle body to the inner surface of the outer nozzle body, the at least one flow affector including an outer surface portion and an inner surface portion that defines an interior chamber having an inlet fluidly connected to the fluid passage and at least two openings fluidically linking the interior chamber and the mixing zone;
• and
• one or more flow tuning elements arranged at the interior chamber upstream of the at least two openings, the at least one flow affector being configured and disposed to condition a fluid passing into the interior chamber to affect a substantially iso-kinetic distribution of the fluid within the interior chamber.