This work presents high-fidelity simulations of the aerodynamic noise characteristics of a forward-flight propeller ingesting turbulent wakes of cylinders. Two cylinders with different diameters are employed to generate turbulent wakes with distinct turbulence intensity and length scales, namely small-scale turbulence (SST) and large-scale turbulence (LST). The lattice Boltzmann–very large-eddy simulation solver, PowerFLOW, coupled to an impermeable surface Ffowcs Williams–Hawkings formulation, is used for the forward-flight propeller configuration, matching that of an earlier experimental study. The aerodynamic results show that SST ingestion preserves a coherent tip–vortex path and confines elevated fluctuations to a limited portion of the blades. In contrast, LST ingestion disrupts the tip–vortex trajectory over a wide azimuth and spreads axial-velocity root-mean-square across the disk. Correspondingly, ingesting SST produces a series of discrete tonal sidebands at
$m\mathrm{BPF}\pm nf_0$ (where
$m, n \in \mathbb{N} = \{1,\, 2,\,3,\, \ldots \}$,
$\textrm{BPF}$ is blade passing frequency and
$f_0$ is the cylinder shedding frequency), while the LST case primarily yields notable noise increases in broadband components with clear haystacking around the blade passing frequency harmonics. Blade-level correlation and modulation intensity analyses confirm that the SST case gives rise to compact amplitude modulation, whereas the larger turbulence length scales in LST lead to redistribution of the turbulent energy via haystacking and broadband humps, linking inflow scale and coherence to the observed noise characteristics and generation mechanism. Hemispherical change in overall sound pressure level maps confirm axis-aligned rises in noise levels with turbulence ingestion. These results establish how the scale and coherence of ingested turbulence are crucial to both the near-wake dynamics and the radiated sound of propellers.