Is this new intake of Airbus and Boeing aircraft's NACA inlet?
Those inlets don't require the NACA duct profile because the openings are presented toward the airflow, being on a sloping surface relative to the freestream.  The NACA profile in those locations serves no useful purpose and is a probably less effective, if anything.
The NACA duct profile was developed for inlets on surfaces that are completely parallel to the airflow, like along the straight sides of a fuselage or nacelle, where the freestream flow just passes on by (like a static port you might say).  They were developed as a low drag alternative to the traditional scoop projecting into the airstream that you would normally have to use in such a location.
The sides of the NACA Profile, induce a change in direction of the ram air free stream without any projections (it's thought that the sides of the ramp act like vortex generators and it's the vortices that &quot;pull&quot; the free stream down the ramp) so that ram air is drawn down the ramp to the inlet opening.  On a sloping surface like a wing root fairing as in those pictures, the ram air is directly impinging on the opening (as if it was a scoop sticking out) and doesn't need any &quot;airflow redirection tricks&quot; like the curved sides on the NACA inlet ramp.