Combustor with dilution openings

A turbine engine comprising:

• a compressor section, a combustion section, and a turbine section in serial flow arrangement along an engine centerline, the combustion section comprising:
• a combustor liner having a first end, a second end, opposing the first end, and at least partially defining a combustion chamber extending between the first end and the second end and defining a combustor length L;
• a dome assembly including a dome wall mounted to the combustor liner at the first end and defining a dome inlet of the combustion chamber;
• multiple sets of dilution holes comprising at least:
• a first set of dilution holes provided in the combustor liner downstream from the dome inlet;
• and
• a second set of dilution holes having at least one physical characteristic that different from the first set of dilution holes and provided in the combustor liner between the first set of dilution holes and the dome inlet, wherein the at least one physical characteristic includes a dilution angle or a dilution flow area.