Hiển thị ở chế độ nhân viên: Nonlinear forced vibration of sandwich cylindrical panel with negative Poisson’s ratio auxetic honeycombs core and CNTRC face sheets

Nonlinear forced vibration of sandwich cylindrical panel with negative Poisson’s ratio auxetic honeycombs core and CNTRC face sheets

Lưu vào:

Hiển thị chi tiết
Tác giả chính:	Nguyen Van Quyen
Đồng tác giả:	Nguyen Van Thanh
Định dạng:	Bài Báo
Ngôn ngữ:	English
Nhà xuất bản:	Thin-Walled Structures 2021
Chủ đề:	Free and forced vibration Auxetic honeycombs structure Carbon nanotube reinforced composite Visco-Pasternak foundations
Truy cập trực tuyến:	https://www.sciencedirect.com/science/article/abs/pii/S0263823121001099?via%3Dihub#! https://dlib.phenikaa-uni.edu.vn/handle/PNK/1951 https://doi.org/10.1016/j.tws.2021.107571
Từ khóa:	Thêm từ khóa Không có từ khóa, Hãy là người đầu tiên đánh dấu biểu ghi này!

id	oai:localhost:PNK-1951
record_format	dspace
spelling	oai:localhost:PNK-19512022-08-17T05:54:53Z Nonlinear forced vibration of sandwich cylindrical panel with negative Poisson’s ratio auxetic honeycombs core and CNTRC face sheets Nguyen Van Quyen Nguyen Van Thanh Tran Quoc Quan Nguyen Dinh Duc Free and forced vibration Auxetic honeycombs structure Carbon nanotube reinforced composite Visco-Pasternak foundations Q1 Recently, auxetic cellular solids in the forms of honeycombs and carbon nanotube reinforced composite (CNTRC) have great potential in a diverse range of applications. This paper studies the nonlinear free and forced vibration of sandwich cylindrical panel on visco-Pasternak foundations in thermal environment subjected to blast load The sandwich cylindrical panel consists of auxetic honeycombs core layer and two CNTRC face sheets. The Poisson’ ratio of the auxetic core is negative and the material properties of CNTRC face sheets are assumed to continuously vary in the thickness direction according to four different types of linear functions. The blast load is determined from the distance of the center of blast to center of the structure and the mass of explosive materials. The fundamental equations are established based on Reddy’s higher order shear deformation shell theory taking into account the effect of initial imperfection and visco-Pasternak foundations. The Galerkin and Runge–Kutta methods are used to obtain the nonlinear dynamic response and the natural frequency of the sandwich cylindrical panel. The numerical results show the effect of geometrical parameters, visco foundations, initial imperfection, temperature increment, nanotube volume fraction and blast load on the nonlinear vibration characteristics of the sandwich cylindrical panel. The accuracy of present approach and theoretical results is verified by some comparisons with the known data in the literature. 2021-07-05T09:35:41Z 2021-07-05T09:35:41Z 2021 Article https://www.sciencedirect.com/science/article/abs/pii/S0263823121001099?via%3Dihub#! https://dlib.phenikaa-uni.edu.vn/handle/PNK/1951 https://doi.org/10.1016/j.tws.2021.107571 en application/pdf Thin-Walled Structures
institution	Digital Phenikaa
collection	Digital Phenikaa
language	English
topic	Free and forced vibration Auxetic honeycombs structure Carbon nanotube reinforced composite Visco-Pasternak foundations
spellingShingle	Free and forced vibration Auxetic honeycombs structure Carbon nanotube reinforced composite Visco-Pasternak foundations Nguyen Van Quyen Nonlinear forced vibration of sandwich cylindrical panel with negative Poisson’s ratio auxetic honeycombs core and CNTRC face sheets
description	Q1
author2	Nguyen Van Thanh
author_facet	Nguyen Van Thanh Nguyen Van Quyen
format	Article
author	Nguyen Van Quyen
author_sort	Nguyen Van Quyen
title	Nonlinear forced vibration of sandwich cylindrical panel with negative Poisson’s ratio auxetic honeycombs core and CNTRC face sheets
title_short	Nonlinear forced vibration of sandwich cylindrical panel with negative Poisson’s ratio auxetic honeycombs core and CNTRC face sheets
title_full	Nonlinear forced vibration of sandwich cylindrical panel with negative Poisson’s ratio auxetic honeycombs core and CNTRC face sheets
title_fullStr	Nonlinear forced vibration of sandwich cylindrical panel with negative Poisson’s ratio auxetic honeycombs core and CNTRC face sheets
title_full_unstemmed	Nonlinear forced vibration of sandwich cylindrical panel with negative Poisson’s ratio auxetic honeycombs core and CNTRC face sheets
title_sort	nonlinear forced vibration of sandwich cylindrical panel with negative poisson’s ratio auxetic honeycombs core and cntrc face sheets
publisher	Thin-Walled Structures
publishDate	2021
url	https://www.sciencedirect.com/science/article/abs/pii/S0263823121001099?via%3Dihub#! https://dlib.phenikaa-uni.edu.vn/handle/PNK/1951 https://doi.org/10.1016/j.tws.2021.107571
_version_	1751856256119734272
score	8.887836

Nonlinear forced vibration of sandwich cylindrical panel with negative Poisson’s ratio auxetic honeycombs core and CNTRC face sheets

Tài liệu tương tự