33th Congress of the International Council of the Aeronautical Sciences

03.3 - Basic Fluid Dynamics and Flow Control

PRELIMINARY STUDY ON A FLUIDIC DEVICE SUPPORTING AIRCRAFT-FLIGHT CONTROL

W. Stalewski, Lukasiewicz Research Network- Institute of Aviation, Poland

A novel fluidic device concept designed to support aircraft control through the control of velocity circulation around an aircraft wing has been developed and pre-investigated based on a computational approach. The device operates based on simultaneous blowing and suction through the mini-nozzles located at the trailing edge of any lifting or control surface of aircraft.


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