06.1 - Flight Dynamics and Control (Control & Modelling)
FREE FLIGHT TEST IN HORIZONTAL WIND TUNNEL WITH POWERED AIRCRAFT
J.-F. Wang¹, S.-G. Lu¹, S. Feng¹, M.-H. Wang¹; ¹AVIC Aerodynamics Research Institute, China
Modern advanced layout aircraft is faced with multi-disciplinary coupling problems such as aerodynamic layout and flight control system design. In order to carry out aerodynamic/flight/control integration research at the early stage of design, shorten the development cycle and reduce the development cost, a model free flight test system was established in 8m×6m open wind tunnel based on similarity criterion.