APPLICATION OF MATHEMATICAL MODELING OF THE AIRCRAFT STRUCTURES STRESS STATE TO OPTIMIZE CORROSION DAMAGE REMOVAL

During the long-term aircraft operation, corrosion damage occurs on the aircraft structure. This leads to reducing of construction strength, rigidity and durability. Due to this corrosion damage removal and paintwork restoration are performed during the maintenance operation. During the corrosion da...

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Bibliographic Details
Main Authors: D. P. Saidzhanov, V. V. Efimov
Format: Article
Language:Russian
Published: Moscow State Technical University of Civil Aviation 2021-02-01
Series:Naučnyj Vestnik MGTU GA
Subjects:
Online Access:https://avia.mstuca.ru/jour/article/view/1789