TY  - JOUR
ID  - SisLab2820
UR  - https://eprints.uet.vnu.edu.vn/eprints/id/eprint/2820/
A1  - Nguyen, Dinh Duc
A1  - Kim, Seung-Eock
A1  - Ngo, Duc Tuan
A1  - Tran, Phuong
Y1  - 2017///
N2  - The main goal of this study is using analytical solution to investigate the nonlinear dynamic response and
vibration of sandwich auxetic composite cylindrical panels. The sandwich composite panels have three
layers in which the top and bottom outer skins are isotropic aluminum materials, the central auxetic
core layer ? honeycomb structures with negative Poisson?s ratio using the same aluminum material. The
panels are resting on elastic foundations and subjected to mechanical, blast and damping loads. Based
on Reddy?s first order shear deformation theory (FSDT) with the geometrical nonlinear in von Karman
and using the Airy stress functions method, Galerkin method and fourth-order Runge?Kutta method,
the resulting equations are solved to obtain expressions for nonlinear motion equations. The effects
of geometrical parameters, material properties, elastic Winkler and Pasternak foundations, mechanical,
blast and damping loads on the nonlinear dynamic response and the natural frequencies of sandwich
composite cylindrical panels are studied.
PB  - Elsevier
JF  - Aerospace Science and Technology
VL  - 70
SN  - 1270-9638
TI  - New approach to study nonlinear dynamic response and vibration of sandwich composite cylindrical panels with auxetic honeycomb core layer
SP  - 396
AV  - public
EP  - 404
ER  -