Zobrazeno 1 - 10 of 18 pro vyhledávání: '"Alexander Shanygin"'
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Akademický článek
Manufacturing Aspects of Creating Low-Curvature Panels for Prospective Civil Aircraft
Autor: Evgeny Dubovikov, Danil Fomin, Natalia Guseva, Ivan Kondakov, Evgeny Kruychkov, Ivan Mareskin, Alexander Shanygin
Publikováno v: Aerospace, Vol 6, Iss 2, p 18 (2019)
For this study, structural and manufacturing schemes for low-curvature pressurized fuselage panels were proposed, making it possible to provide high weight efficiency for the airframes of prospective civil blended wing-body (BWB) aircraft. The manufa
Externí odkaz: https://doaj.org/article/8e008806931f4a8bb7e858f0b427b535
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5
Development of rational hybrid fuselage structure for prospective civil aircraft
Autor: I Kondakov, Alexander Shanygin, E. Dubovikov, D Vedernikov, V. Fomin
Publikováno v: Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering. 232:2673-2680
The concept of hybrid fuselage structure including conventional metal, conventional composite, and lattice composite sections is presented. The method of strength analysis and choosing the rational values of structure parameters of hybrid fuselage st
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::65c1a5227078bd9ba2475c91e58fcedb
https://doi.org/10.1177/0954410018785501
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6
Lightweight and reliable metal–composite joints based on harmonization of strength properties of joined parts
Autor: Alexander Shanygin, Andrey Chernov, Ivan Mareskin, Ivan Kondakov, Danil Fomin
Publikováno v: Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering. 232:2663-2672
One of the key problems of designing composite primary aircraft structures is the problem of development of lightweight and reliable joints for such structures. For conventional bolted joints used for connection of laminated composite primary structu
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::eb0f42fb6a72bc84f0bd8cb7bfa22be6
https://doi.org/10.1177/0954410018778797
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9
Manufacturing Aspects of Creating Low-Curvature Panels for Prospective Civil Aircraft
Autor: Danil Fomin, Natalia Guseva, Alexander Shanygin, Ivan Mareskin, Evgeny Dubovikov, Ivan Kondakov, Evgeny Kruychkov
Publikováno v: Aerospace
Volume 6
Issue 2
Aerospace, Vol 6, Iss 2, p 18 (2019)
For this study, structural and manufacturing schemes for low-curvature pressurized fuselage panels were proposed, making it possible to provide high weight efficiency for the airframes of prospective civil blended wing-body (BWB) aircraft. The manufa
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::9e36df07a7d3fedcee988b0972527bfd
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10
High resolution ply-by-ply ultrasound imaging of impact damage in thick CFRP laminates by high-frequency acoustic microscopy
Autor: Andrey Chernov, Vadim Levin, Egor Morokov, Alexander Shanygin
Publikováno v: Composite Structures. 256:113102
Impact behavior of the carbon fiber reinforced polymers (CFRP) is still actual issue despite long history of laminate application and investigation of impact resistance. Expansion of knowledge on fracture mechanisms in reinforced composites could be
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::b6fedc92bb01fa3e746af26b3b381d0e
https://doi.org/10.1016/j.compstruct.2020.113102
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