Dual-mode exit area scheduling refers to an automatic control system that adjusts the engine's exit area based on flight conditions and thrust demands. This system enhances engine performance by allowing supersonic flow and increasing exhaust velocity during critical phases like takeoff. The "dual mode" likely indicates redundant computer controls managing this scheduling process. Discussions also touch on the F-16's nozzle controls, specifically the A8 and A9 areas, which pertain to the throat and exit areas of the nozzle. Understanding these systems is crucial for optimizing aircraft performance, especially during supersonic maneuvers.