Turbine engine with fuel nozzle assembly

A turbine engine comprising:

• a compressor section, combustor section, and turbine section in serial flow arrangement, with the combustor section including a fuel nozzle assembly comprising:
• an annular swirler;
• and
• a fuel nozzle having an outer wall and an outlet, the fuel nozzle defining a longitudinal axis and extending through the annular swirler, the fuel nozzle comprising:
• a primary passage arranged centrally within the fuel nozzle;
• an outer passage arranged within the fuel nozzle exterior of the primary passage;
• an intermediate passage positioned within the fuel nozzle exterior of the primary passage and interior of the outer passage;
• and
• an opening extending through the outer wall and exhausting to the intermediate passage.