On the Buccaneer the standard procedure was to open the brakes in stages around the circuit until they were fully open on finals. This ensured the engines could be run at high enough RPM to generate bleed air for the boundary layer blowing system, without the aircraft accelerating. This also, as mentioned already, had the desirable side effect of allowing a rapid go round as the engines would already be at around 80-90% so wouldn't take long to accelerate to max continuous power while the brakes were closed.
On the Vixen the pilot's notes include checking the brake is retracted as part of the pre-landing checks. The wing on the Vixen allowed quite a low stall speed so it didn't need the same help the Buccaneers did and relatively low power settings could be used, of course the position of the brake on the Vixen also meant it couldn't be fully extended with the gear down so it would have been of limited help anyway.
Incidentally, air brakes don't necessarily disturb laminar flow and kill lift, if they don't form part of the wing surface, a la the Phantom, there won't be any lift being generated to kill. So in the case of the Buccaneer or the F-105 where the tail section or afterburner petals opened up the only alteration in lift would be due to the change in speed.