Zobrazeno 1 - 7
of 7
pro vyhledávání: '"Evgeny E. Maslov"'
Publikováno v:
Aerospace, Vol 6, Iss 3, p 25 (2019)
A complex modeling technique is presented in this paper for a numerical analysis of compressed stiffened composite panels with impact damage. The numerical technique is based on the LS-Dyna code application, which simulates both the dynamic deformati
Externí odkaz:
https://doaj.org/article/c51ea60b92f44abbaa90c4bfb0b4a31f
Autor:
Evgeny E. Maslov, S. S. Kukanov, D. Yu. Strelets, V. I. Romanov, M. A. Pogosyan, M. S. Litvinov, A. A. Ryabov
Publikováno v:
Aerospace Systems. 2:155-161
The manuscript discusses issues related to the use of mathematical modeling to substantiate the reliability and safety of the Superjet-100 aircraft during the emergency landing. The problem of the passenger airplane airframe dynamic deformation in th
Publikováno v:
Multiscale Solid Mechanics ISBN: 9783030549275
The results of numerical and experimental investigations are presented in the paper for impulse loading of cylindrical shell of constant thickness subjected to shock wave of spherical charge explosion of different trinitrotoluol equivalent (TNT). Num
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::744fbbf2801dc365bb8f8352081c3de6
https://doi.org/10.1007/978-3-030-54928-2_5
https://doi.org/10.1007/978-3-030-54928-2_5
Autor:
Evgeny E. Maslov, V. G. Slobodchikov, D. Yu. Strelets, Jsc 'AeroKompozit', Moscow, Russian Federation, A. A. Ryabov
Publikováno v:
Problems of Strength and Plasticity. 80:90-97
The results of numerically analyzing a stringer-stiffened multilayer composite panel under local dynamic loading, followed by axial quasi-static compression of the damaged panel with slowly increasing longitudinal loading, are presented. The analysis
Publikováno v:
Aerospace
Volume 6
Issue 3
Aerospace, Vol 6, Iss 3, p 25 (2019)
Volume 6
Issue 3
Aerospace, Vol 6, Iss 3, p 25 (2019)
A complex modeling technique is presented in this paper for a numerical analysis of compressed stiffened composite panels with impact damage. The numerical technique is based on the LS-Dyna code application, which simulates both the dynamic deformati
Publikováno v:
Aerospace (MDPI Publishing); Mar2019, Vol. 6 Issue 3, p25-25, 1p
This book provides an overview of the current of the state of the art in the multiscale mechanics of solids and structures. It comprehensively discusses new materials, including theoretical and experimental investigations their durability and strengt