The effect of perforation on the wake of a thin flat plate placed normal to the free stream at Reynolds number (
$Re$
) 250 (based on plate width
$d$
, and inflow velocity
$U_o$
) is studied by means of direct numerical simulation. The perforated plate of length
$6d$
consist of six equidistant square holes of varying sizes corresponding to porosity
$\beta$
(ratio of open area to total plate area) of 0 %, 4 %, 9 %, 12.25 %, 16 %, 20.25 % and 25 %. It is observed that the bleed or jet flow through perforations pushes the shear layer interaction farther downstream with increasing
$\beta$
. This causes a monotonic decrease in the drag coefficient with increasing porosity, and a sharp fall seeming to begin at
$\beta \approx 4\,\%$
. On the other hand, the Strouhal number increases with
$\beta$
up to 16 % (at
$\beta =16\,\%$
, loss of flow three-dimensionality leads to a ‘quasi-laminar’ state of flow). This is followed by a sharp fall in the Strouhal number at
$\beta \approx 20\,\%$
. The behaviour of the large-scale vortical structures in the far wake is influenced by the near-wake behaviour of the bleed flow, where the local
$Re$
based on the perforation hole size determines the overall flow three-dimensionality. It is also observed that the jet or bleed flow undergoes meandering instability when pitch separation is equivalent to the hole size (at
$\beta =25\,\%$
). The low-
$Re$
turbulent flow for a non-perforated plate is altered to a transitional state by the presence of perforation. The streamwise vortex pairs (secondary instabilities) become fairly organized as
$\beta$
is increased from 0 % to 16 %. The secondary instability at
$\beta =16\,\%$
appears similar to mode-B with wavelength
${\approx }1d$
. On the contrary, the secondary instability at
$\beta =25\,\%$
appears similar to mode-A with a wavelength of
${\approx }2d$
.