Активная система управления обтеканием закрылка на модели отсека крыла пассажирского самолета

In this work, a model of an active system for controlling the wing flap flow was designed and manufactured. The presented active flow control system operates by blowing air under pressure onto the upper surface of the flap. The system consists of a device supplying compressed air to the flap and the flap leading edge, through which the air is blown out. For experimental testing, the system was built into the existing large-scale aerodynamic model of a mechanized wing compartment.