04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity
AEROSERVOELASTIC OPTIMIZATION OF A HIGH ASPECT TRANSPORT WING WITH MORPHING TRAILING EDGE
Z.-K. Zhang¹, Y.-J. Yang¹, S. Ricci², A. De Gaspari², C. Song¹, C. Yang¹; ¹Beihang University, China ;²Politecnico di Milano, Italy
To better understand the aeroelastic behavior of the high aspect wing with morphing trailing edge, this paper will conduct the research on aeroelastic analysis and aeroservoelastic optimization for a subsonic transport wing, the geometry non-linearity and dynamic behavior of morphing trailing edge itself will be taken into account.