27th Congress of International Council of the Aeronautical Sciences, 19 - 24 September 2010, Nice, France
Paper ICAS 2010-9.8.3

THE DEVELOPMENT OF 3 DOF WING SECTION MODEL FOR AEROELASTIC AND ACTIVE CONTROL WIND TUNNEL EXPERIMENTAL TESTS

R. A. Sasongko, L. Gunawan, M. Akbar
Institute of Technology Bandung, Indonesia

Keywords: aeroelasticity, wind-tunnel test, flutter

This paper discusses the analysis for developing a wind tunnel equipment for investigating a 3 D.o.F aeroelastic system. The equipment is designed such that the desired aeroelastic phenomena can be observed. The results covered in this paper can be used for the development of the physical equipment.

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