“…, at near critical conditions), whose growth is still close to zero, and the shape of streamlines and disturbed interface are similar to those of longer wave perturbations (see details in Barmak et al, 2016b). It is important to mention that the flow is not steady with respect to the stationary frame of reference (which is used in the present study), and the (moving) interface at a particular moment of time may not coincide with a streamline (Figures 7(b), (d), (f), see details in Barmak et al, 2016b). Figures 7(a), (c), (e), the perturbations are represented by pairs of antisymmetric vortices (of /2 wave l width) with their core, i.e., the maximum of the stream function perturbations, located in the bulk of air layer (A and C) or at the interface (B).…”