27th Congress of International Council of the Aeronautical Sciences, 19 - 24 September 2010, Nice, France
Paper ICAS 2010-9.4.2

COMBINED SCALAR AND VECTOR VELOCITY POTENTIAL FOR UNSTEADY AERODYNAMICS IN ACOUSTO-AEROELASTICITY

H. Djojodihardjo
Univ. Al Azhar, Indonesia & Univ. Putra, Malaysia,

Keywords: unsteady aerodynamics, acousto-aeroelasticity, fluid structure interaction, boundaryelement method

Unified Boundary-Element treatment of the combined acousto-aeroelastic problem, by using the velocity field contributed by the irrotational flow field as well as the rotational part contributed by the viscous layer. The lifting surface approach for the aerodynamic problem will be substituted by using direct boundary integral approach

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