Dynamic Response of Moderately Thick Cylindrical Panels

AIAA Journal ◽  
1972 ◽  
Vol 10 (5) ◽  
pp. 565-566 ◽  
Author(s):  
TIEN-YU TSUI
2017 ◽  
Vol 21 (8) ◽  
pp. 2816-2845 ◽  
Author(s):  
Nguyen D Duc ◽  
Ngo Duc Tuan ◽  
Phuong Tran ◽  
Tran Q Quan ◽  
Nguyen Van Thanh

This study follows an analytical approach to investigate the nonlinear dynamic response and vibration of eccentrically stiffened sandwich functionally graded material (FGM) cylindrical panels with metal–ceramic layers on elastic foundations in thermal environments. It is assumed that the FGM cylindrical panel is reinforced by the eccentrically longitudinal and transversal stiffeners and subjected to mechanical and thermal loads. The material properties are assumed to be temperature dependent and graded in the thickness direction according to a simple power law distribution. Based on the Reddy’s third-order shear deformation shell theory, the motion and compatibility equations are derived taking into account geometrical nonlinearity and Pasternak-type elastic foundations. The outstanding feature of this study is that both FGM cylindrical panel and stiffeners are assumed to be deformed in the presence of temperature. Explicit relation of deflection–time curves and frequencies of FGM cylindrical panel are determined by applying stress function, Galerkin method and fourth-order Runge-Kutta method. The influences of material and geometrical parameters, elastic foundations and stiffeners on the nonlinear dynamic and vibration of the sandwich FGM panels are discussed in detail. The obtained results are validated by comparing with other results in the literature.


2018 ◽  
Vol 22 (3) ◽  
pp. 658-688 ◽  
Author(s):  
Nguyen Dinh Duc ◽  
Ngo Duc Tuan ◽  
Pham Hong Cong ◽  
Ngo Dinh Dat ◽  
Nguyen Dinh Khoa

Based on the first order shear deformation shell theory, this paper presents an analysis of the nonlinear dynamic response and vibration of imperfect eccentrically stiffened functionally graded material (ES-FGM) cylindrical panels subjected to mechanical, thermal, and blast loads resting on elastic foundations. The material properties are assumed to be temperature-dependent and graded in the thickness direction according to simple power-law distribution in terms of the volume fractions of the constituents. Both functionally graded material cylindrical panels and stiffeners having temperature-dependent properties are deformed under temperature, simultaneously. Numerical results for the dynamic response of the imperfect ES-FGM cylindrical panels with two cases of boundary conditions are obtained by the Galerkin method and fourth-order Runge–Kutta method. The results show the effects of geometrical parameters, material properties, imperfections, mechanical and blast loads, temperature, elastic foundations and boundary conditions on the nonlinear dynamic response of the imperfect ES-FGM cylindrical panels. The obtained numerical results are validated by comparing with other results reported in the open literature.


2020 ◽  
Vol 146 ◽  
pp. 106438 ◽  
Author(s):  
Nguyen Dinh Duc ◽  
Seung-Eock Kim ◽  
Duong Tuan Manh ◽  
Pham Dinh Nguyen

Author(s):  
Srinivasa D. Thoppul ◽  
Judah Ari-Gur

The dynamic response of plates and cylindrical panels with various curvatures under external lateral pressure pulse was studied. Nonlinearities due to large deflections were included and the dynamic response was analyzed using a finite element code. Effects of shell curvatures, pulse durations and load intensities were investigated. The observed dynamic behavior included also non-linear shell buckling due to the compressive stresses under the external pressure on the cylindrical panels. The results, when compared to the linear response, show the effects of the increased load intensity and the resulting non-linear behavior on the response to various pulse durations. Also, the differences between the static and the dynamic behaviors for similar load intensities were studied. Non-dimensional processing of the results, including in the large deflection range, highlights the effects of high load intensities on the structural stiffness and in turn on the changing characteristics of the response under a given pulse duration.


Author(s):  
Edward Seckel ◽  
Ian A. M. Hall ◽  
Duane T. McRuer ◽  
David H. Weir
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