30th Congress of the International Council of the Aeronautical Sciences

03.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity

DESIGN, MANUFACTURE AND FREQUENCY EXPERIMENT OF A NOVEL FLUTTER MODEL FOR AGARD WING 445.6 WITH STRUCTURE-SIMILARITY

W. Qian¹, Y.-G. Bai¹, D. Wang, AVIC Aerodynamics Research Institute, China; ¹Dalian University of Technology, China

No.3 model with weak stiffness was modelled. A reference flutter model of AGARD WING 445.6 was design and manufactured. A frequency experiment, modal analysis and flutter computation of this model was completed. It was found the proposed model can satisfy the requirement of the temporary impulse wind tunnel in China.


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