26th Congress of International Council of the Aeronautical Sciences
including the 8th AIAA Aviation Technology, Integration, and Operations (ATIO) Conference
14 - 19 September 2008, Anchorage, Alaska, USA
Paper ICAS 2008-7.7.3

UNIFIED BE-FE AERODYNAMIC-ACOUSTIC-STRUCTURE COUPLING SCHEME FOR ACOUSTIC EFFECTS ON AEROELASTIC STRUCTURES

H. Djojodihardjo
Universitas Al-Azhar (Indonesia) & Universiti Sains, Malaysia

Keywords: aeroacoustoelasticity, fluid structure interaction, active flutter control

Combined acoustic and aerodynamic loading on the structure is treated using linear superposition of the acoustic pressure disturbance to the aeroelastic problem and treatment of the acoustic pressure as motion independent and motion dependent acoustic pressure. The aerodynamic loading can also be formulated using Green’s function approach.

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