K.Balunov, V.Chedrik, F.Ishmuratov

DOI Number: N/A

Conference number: IFASD-2017-011

The paper is devoted to aero-structural optimization of aircraft wing based on a multidisciplinary approach. The focus is on the study of influence of elastic, inertial and aerodynamic forces on optimal shape and structural parameters of the wing tip part. Main features of the proposed bi-level method are presented. Numerical results of structural optimization for middle range civil aircraft are discussed.

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In Categories: 1.Events, Aeroelasticity in Conceptual Aircraft Design, IFASD 2017
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