Zobrazeno 1 - 5
of 5
pro vyhledávání: '"Ivan Mareskin"'
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
Autor:
Alexander Shanygin, A. A. Babichev, Ivan Mareskin, V. V. Vasiliev, A. A. Skleznev, D. Yu. Fomin, A. F. Razin
Publikováno v:
Composite Materials Constructions. :3-6
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
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)
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
Publikováno v:
MATEC Web of Conferences, Vol 304, p 01019 (2019)
The paper is devoted to the creation of automated methods for calculating the strength of composite structures, taking into account the influence of impact damage and temperature effects in the range from -600 to +600. To solve this problem, a progra