APPLICATION OF MATHEMATICAL MODELING OF THE AIRCRAFT STRUCTURES STRESS STATE TO OPTIMIZE CORROSION DAMAGE REMOVAL
https://doi.org/10.26467/2079-0619-2021-24-1-49-61
Abstract
About the Authors
D. P. SaidzhanovRussian Federation
Postgraduate Student, Aerodynamics, Airframe and Strength of Aircraft Chair
Moscow
V. V. Efimov
Russian Federation
Doctor of Technical Sciences, Associate Professor, Professor of Aerodynamics, Airframe and Strength of Aircraft Chair
Moscow
References
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Review
For citations:
Saidzhanov D.P., Efimov V.V. APPLICATION OF MATHEMATICAL MODELING OF THE AIRCRAFT STRUCTURES STRESS STATE TO OPTIMIZE CORROSION DAMAGE REMOVAL. Civil Aviation High Technologies. 2021;24(1):49-61. (In Russ.) https://doi.org/10.26467/2079-0619-2021-24-1-49-61