04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity
AEROELASTIC ANALYSIS OF HIGH ASPECT RATIO AND STRUT-BRACED WINGS
Y. Le Lamer¹, J. Morlier, ICA, Université de Toulouse, ISAE-SUPAERO, MINES ALBI, UPS, INSA, France; E. Benard¹, P. He, Iowa State University, United States; ¹ISAE-SUPAERO, Université de Toulouse, France
Increasing the aspect ratio of transonic aircraft wings is a promising path to reduce aviation carbon footprint. This paper focuses on the development of high and low fidelity aeroelastic models for high aspect ratio and strut-braced wings. These models are implemented within an aeroelastic analysis framework. Finally, high and low fidelity analysis will be performed and results compared.