Direct Numerical Simulations of the injection of a pulsed round liquid jet in a stagnant gas are performed in a series of runs of geometrically progressing resolution.
The Reynolds and Weber numbers and the density ratio are sufficiently large for reaching a complex high-speed atomization regime but not so large so that the small length scales of the flow are impossible to resolve, except for very small liquid-sheet thickness.
The Weber number based on grid size is then small, an indication that the simulations are very well resolved. Computations are performed using octree adaptive mesh refinement with a finite volume method and height-function computation of curvature, down to a specified minimum grid size
This non-convergence arises from the {\em numerical sheet breakup} effect, in which the interface becomes rough just before it breaks.
The rough appearance of the interface is associated to a high-wavenumber oscillation of the curvature.
To recover convergence, we apply the controlled ``manifold death'' numerical procedure, in which thin sheets are detected, and then pierced by fiat before they reach a set critical thickness
This allows convergence of the droplet frequency above a certain critical diameter
A unimodal distribution is observed in the converged range.