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pro vyhledávání: '"I. O. Kondakov"'
Autor:
I. O. Kondakov
Publikováno v:
Научный вестник МГТУ ГА, Vol 19, Iss 6, Pp 137-146 (2017)
Lattice composite fuselage structures are developed as an alternative to conventional composite structures based on laminated skin and stiffeners. Structure layout of lattice structures allows to realize advantages of current composite materials to a
Externí odkaz:
https://doaj.org/article/3fa137707dc34159ba8468fe204b2e22
Publikováno v:
Научный вестник МГТУ ГА, Vol 19, Iss 6, Pp 127-136 (2017)
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 b
Externí odkaz:
https://doaj.org/article/8b972413983a46bdb5b8f929e9d14fba
Publikováno v:
Mechanics of Composite Materials. 57:721-730
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::18186ed5cc7dd204dca970ae89a5ca13
https://doi.org/10.1007/s11029-022-09994-1
https://doi.org/10.1007/s11029-022-09994-1