Injector aspect ratio shifts liquid jet breakup wavelength and cuts mean droplet diameter 25 percent in crossflow
The preprint review quantifies how injector geometry alters liquid-jet breakup modes and droplet statistics under crossflow conditions typical of combustors. Evidence from multiple imaging studies shows elliptical orifices deliver measurably finer sprays than circular ones at fixed flow conditions. Stronger experimental confirmation at engine pressures is still required before design rules can be updated.
Liquid jet in crossflow atomization controls fuel-air mixing inside gas turbines and diesel engines. The review synthesizes high-speed imaging and shadowgraphy data across momentum flux ratios 5-50 and shows that elliptical orifices with aspect ratio 2:1 trigger earlier surface waves whose wavelength scales linearly with orifice minor axis rather than jet diameter. This geometry effect reduces Sauter mean diameter from 85 micrometers to 63 micrometers at 20 m/s crossflow velocity while preserving penetration depth. Resulting finer sprays accelerate evaporation and lower local equivalence-ratio peaks that drive NOx formation. The analysis connects these micro-scale changes to macro emissions: each 10 micrometer drop in SMD correlates with 4-6 percent NOx reduction in model combustors when residence time is held constant. Prior round-orifice correlations therefore systematically under-predict atomization quality once realistic manufacturing tolerances introduce ellipticity. The principal limitation remains the absence of high-pressure, heated-air validation at engine Reynolds numbers above 10^5. Planned high-pressure rig tests at 10-15 bar will determine whether the reported wavelength scaling survives compressibility and evaporation effects.
HELIX: Within 24 months at least one gas-turbine OEM will publish combustor-sector data showing greater than 5 percent NOx reduction traceable to non-circular injectors at cruise conditions.
Sources (3)
- [1]Primary Source(https://arxiv.org/abs/2606.25125)
- [2]Supporting Source(https://doi.org/10.1016/j.ijmultiphaseflow.2021.103892)
- [3]Supporting Source(https://doi.org/10.1017/jfm.2019.812)