04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity
DEVELOPMENT OF LIGHTWEIGHT HYBRID AIRFRAMES BASED ON UNIDIRECTIONAL COMPOSITE STRUCTURE CONCEPTS
A. Shanygin, Russia
In this work the results of the investigations of hybrid structures of the new generation. The main feature of such hybrid structure is not only presence of metallic and composite parts, but also the presence of a considerable transition zones, integrating both composite and metallic elements. For substantiation of effectiveness of such structures the results of weight analysis are presented.