Aircraft engine noise can be reduced by applying various design strategies and technologies that target the different sources and characteristics of noise. For example, fan design can be optimized by altering blade geometry, number, spacing, sweep, fan speed, and diameter. This can reduce the fan tip speed and noise generated by the blade passing frequency. Additionally, a shroud or duct around the fan can improve aerodynamic performance and reduce noise radiation. Jet design can be modified by changing jet shape, speed, temperature, pressure, nozzle geometry, and configuration. Decreasing jet speed and increasing jet temperature and pressure can lower Mach number and turbulent kinetic energy to reduce jet noise. Adding chevrons, lobes, or slots to the nozzle enhances mixing and spreading of the jet flow to reduce noise. Combustion design controls fuel type, mixture, injection, ignition, chamber geometry, and pressure. Using lean or alternative fuels and adjusting fuel-air ratio and injection timing stabilizes flame and minimizes pressure fluctuations to reduce combustion noise. Liners, baffles, or dampers in the chamber absorb or dissipate acoustic energy to reduce combustion noise. Turbine design optimizes blade geometry, number, spacing, sweep, turbine speed, and diameter to lower blade passing frequency and shock wave formation. Placing a silencer or diffuser after the turbine expands and slows down gas flow to reduce turbine noise.