30th Congress of the International Council of the Aeronautical Sciences

03.2 - Structural Analysis and Design, Structural Dynamics, Aeroelasticity

FLUID-STRUCTURE INTERACTION ANALYSIS REGARDING THE INFLUENCE OF STRUCTURAL BOUNDARY CONDITION ON A FLAPPING WING

H. Cho¹, N. Lee², S.J. Shin¹, S. Lee², S.Y. Kim, Agency for Defense Development, South Korea; ¹Seoul National Univ., South Korea ;²Inha Univ., South Korea

In this paper, the FSI analysis framework for flapping wing is developed. And, nonlinear shell element based on the CR framework is developed. By using the present shell element, the FSI analysis for flapping wing will be conducted.


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