06.1 - Flight Dynamics and Control (Control & Modelling)
RAPID PROTOTYPING IN AIRCRAFT DESIGN USING CFD, WIND TUNNEL AND FLIGHT TESTING
R. Larsson¹, U. Ringertz, Royal Institute of Technology, KTH, Sweden; D. Lundström, Linköping University, LIU, Sweden; A. Sobron¹; ¹Saab Aeronautics, Sweden
This paper describes the process and methods used for rapid prototyping, sub-scale flight-testing and analysisrnof an aircraft design. New wings have been designed for a radio controlled flying demonstrator. The resultsrncan be used in education and research to further enhance and explore the field of Aeronautical engineering.