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Buckling of a Ring-Stiffened Cylindrical Shell Under the External Pressure. / Filippov, Sergei B.; Nesterchuk, Grigory A.

Advanced Structured Materials. Springer Nature, 2022. стр. 49-61 (Advanced Structured Materials; Том 151).

Результаты исследований: Публикации в книгах, отчётах, сборниках, трудах конференцийглава/разделнаучнаяРецензирование

Harvard

Filippov, SB & Nesterchuk, GA 2022, Buckling of a Ring-Stiffened Cylindrical Shell Under the External Pressure. в Advanced Structured Materials. Advanced Structured Materials, Том. 151, Springer Nature, стр. 49-61. https://doi.org/10.1007/978-3-030-87185-7_5

APA

Filippov, S. B., & Nesterchuk, G. A. (2022). Buckling of a Ring-Stiffened Cylindrical Shell Under the External Pressure. в Advanced Structured Materials (стр. 49-61). (Advanced Structured Materials; Том 151). Springer Nature. https://doi.org/10.1007/978-3-030-87185-7_5

Vancouver

Filippov SB, Nesterchuk GA. Buckling of a Ring-Stiffened Cylindrical Shell Under the External Pressure. в Advanced Structured Materials. Springer Nature. 2022. стр. 49-61. (Advanced Structured Materials). https://doi.org/10.1007/978-3-030-87185-7_5

Author

Filippov, Sergei B. ; Nesterchuk, Grigory A. / Buckling of a Ring-Stiffened Cylindrical Shell Under the External Pressure. Advanced Structured Materials. Springer Nature, 2022. стр. 49-61 (Advanced Structured Materials).

BibTeX

@inbook{1925b1ff1856465a86cc319e70822c85,
title = "Buckling of a Ring-Stiffened Cylindrical Shell Under the External Pressure",
abstract = "In this paper, the problem of buckling of a thin elastic cylindrical shell supported by the rings of various stiffness is considered. The Rayleigh–Ritz method is used to obtain the problem{\textquoteright}s analytical solution for the case of the simply supported edges of the shell. The parameters of the optimal distribution of the structure mass between the shell and the stiffening ribs, which is required to maximize the critical pressure, have been found. The solution of the problem of minimizing the mass of a structure at a given critical pressure is obtained. Here are considered the rings with zero eccentricity. The approximate analytical solutions are compared with the numerical solutions obtained by the finite element method.",
keywords = "Asymptotic and Rayleigh–Ritz methods, Buckling, Comsol software package, Optimal parameters, Ring-stiffened shell",
author = "Filippov, {Sergei B.} and Nesterchuk, {Grigory A.}",
note = "Publisher Copyright: {\textcopyright} 2022, The Author(s), under exclusive license to Springer Nature Switzerland AG.",
year = "2022",
doi = "10.1007/978-3-030-87185-7_5",
language = "English",
series = "Advanced Structured Materials",
publisher = "Springer Nature",
pages = "49--61",
booktitle = "Advanced Structured Materials",
address = "Germany",

}

RIS

TY - CHAP

T1 - Buckling of a Ring-Stiffened Cylindrical Shell Under the External Pressure

AU - Filippov, Sergei B.

AU - Nesterchuk, Grigory A.

N1 - Publisher Copyright: © 2022, The Author(s), under exclusive license to Springer Nature Switzerland AG.

PY - 2022

Y1 - 2022

N2 - In this paper, the problem of buckling of a thin elastic cylindrical shell supported by the rings of various stiffness is considered. The Rayleigh–Ritz method is used to obtain the problem’s analytical solution for the case of the simply supported edges of the shell. The parameters of the optimal distribution of the structure mass between the shell and the stiffening ribs, which is required to maximize the critical pressure, have been found. The solution of the problem of minimizing the mass of a structure at a given critical pressure is obtained. Here are considered the rings with zero eccentricity. The approximate analytical solutions are compared with the numerical solutions obtained by the finite element method.

AB - In this paper, the problem of buckling of a thin elastic cylindrical shell supported by the rings of various stiffness is considered. The Rayleigh–Ritz method is used to obtain the problem’s analytical solution for the case of the simply supported edges of the shell. The parameters of the optimal distribution of the structure mass between the shell and the stiffening ribs, which is required to maximize the critical pressure, have been found. The solution of the problem of minimizing the mass of a structure at a given critical pressure is obtained. Here are considered the rings with zero eccentricity. The approximate analytical solutions are compared with the numerical solutions obtained by the finite element method.

KW - Asymptotic and Rayleigh–Ritz methods

KW - Buckling

KW - Comsol software package

KW - Optimal parameters

KW - Ring-stiffened shell

UR - http://www.scopus.com/inward/record.url?scp=85122464257&partnerID=8YFLogxK

UR - https://www.mendeley.com/catalogue/b2687e3e-c92e-3c8c-b04d-8eb7a37d92e0/

U2 - 10.1007/978-3-030-87185-7_5

DO - 10.1007/978-3-030-87185-7_5

M3 - Chapter

AN - SCOPUS:85122464257

T3 - Advanced Structured Materials

SP - 49

EP - 61

BT - Advanced Structured Materials

PB - Springer Nature

ER -

ID: 93174489