NOVEL APPROACH TO DESIGN OF LIGHTWEIGHT AND RELIABLE COMPOSITE PRIMARY AIRCRAFT STRUCTURES

NOVEL APPROACH TO DESIGN OF LIGHTWEIGHT AND RELIABLE COMPOSITE PRIMARY AIRCRAFT STRUCTURES

The experience of construction of composite primary aircraft structures has approved that the weight decrease for composite aggregates of aircraft in comparison with metallic analogues cannot be obtained within the frames of conventional structures based on stiffened laminated composite skin. One of...

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Bibliographic Details
Main Authors: M. Ch. Zichenkov, I. O. Kondakov, A. N. Shanygin
Format: Article
Language:Russian
Published: Moscow State Technical University of Civil Aviation 2017-01-01
Series:Научный вестник МГТУ ГА
Subjects:
aircraft design
composite aircraft structures
composite materials
hybrid aircraft structures
Online Access:https://avia.mstuca.ru/jour/article/view/994
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