Bending of Thick Rectangular Plates with Different Boundaries under Concentrated Load

2010 ◽  
Vol 163-167 ◽  
pp. 1440-1444
Author(s):  
Ying Jie Chen ◽  
Gang Li ◽  
Zhen Xian Zhang ◽  
Bao Lian Fu

Reciprocal theorem method (RTM) is generalized to solve the problem of bending of thick rectangular plate under concentrated load with four edges fixed and with two opposite edges fixed, the third edge simply supported, and the fourth edge free based on Reissner’s theory. The analytical solutions of the thick plate are given, and the relevant date and diagram are given to guidance engineering application.

2012 ◽  
Vol 594-597 ◽  
pp. 2659-2663
Author(s):  
Dan Zhang

According to reciprocal-theorem method (RTM), the deflection equations of thick rectangular plate with two edges simply supported and two edges free under concentrated load are obtained in this paper. Simultaneously through the programming computation, the numerical results with actual value are obtained, which further showed the accuracy and superiority of RTM to solve the bending of thick rectangular plates.


2021 ◽  
Vol 4 (1) ◽  
pp. 13-23
Author(s):  
Festus C. Onyeka ◽  
Thompson E. Okeke

This work studied the critical load analysis of rectangular plates, carrying uniformly distributed loads utilizing direct variational energy calculus. The aim of this study is to establish the techniques for calculating the critical lateral imposed loads of the plate before deflection attains the specified maximum threshold, qiw as well as its corresponding critical lateral imposed load before the plate reaches an elastic yield point. The formulated potential energy by the static elastic theory of the plate was minimized to get the shear deformation and coefficient of deflection. The plates under consideration are clamped at the first and second edges, free of support at the third edge and simply supported at the fourth edge (CCFS). From the numerical analysis obtained, it is found that the critical lateral imposed loads (qiw and qip) increase as the thickness (t) of plate increases, and decrease as the length to width ratio increases. This suggests that as the thickness increases, the allowable deflection improves the safety of the plate, whereas an increase in the span (length) of the plate increases the failure tendency of the plate structure.


2011 ◽  
Vol 105-107 ◽  
pp. 611-614
Author(s):  
Bo Hu ◽  
Rui Li

The exact bending solutions of moderately thick rectangular plates with two opposite sides simply supported are derived based on the symplectic geometry method. The basic equations for the plates are transferred into Hamilton canonical equations. Then the whole state variables are separated. According to the method of eigenfunction expansion in the symplectic geometry, the exact bending solutions of the plates are obtained. Since only the basic elasticity equations of the plates are used and there is no need to select the deformation functions arbitrarily, the approach utilized is completely reasonable.


1944 ◽  
Vol 11 (3) ◽  
pp. A134-A139
Author(s):  
G. F. Carrier

Abstract The problem of evaluating the bending moments, existing in a uniformly loaded clamped plate having the form of a sector of a ring, is one which arises in connection with the stress analysis of reinforced piston heads and in other design problems. In this paper, expressions are derived for the bending moments along the edges of such a plate. Similar problems, i.e., those of the clamped rectangular plate under uniform pressure, under a central concentrated load, and that of the simply supported sector of a disk under uniform pressure, have been discussed by previous authors. The general approach used in the foregoing problems is adopted in the present case; a considerable reduction in the computational work is achieved, however, by the use of an integral-equation method of solving the boundary-condition equations. Numerical results are obtained for plates of various dimensions, and the edge moment distributions are plotted for these cases. Curves are also plotted which indicate the relationship existing between the maximum bending moments derived for sectorial plates and those previously obtained for clamped rectangular plates of similar size.


2020 ◽  
pp. 2-2
Author(s):  
O. M. IBEARUGBULEM ◽  
F. C. ONYEKA ◽  
V.A. BALOGUN ◽  
JOHN. WASIU ◽  
S. E. NNOCHIRI

Due to enormous application of thick plate and its relevance in engineering, various theories for plate analysis have been developed using linear strain–displacement expressions. It is proven from previous studies that results obtained using linear strain–displacement expressions may be unreliable for nonlinear stress and bending analyses. In the present paper, nonlinear strain– displacement expressions are employed for rectangular plates subjected to uniform distributed loads to suggest a more reliable refined plate theory that satisfies the continuity of all of the transverse stress components. This theory, which is based on traditional third-order shear deformation theory of plate is presented and applied in a bending analysis of rectangular thick plate. Governing equations and associated boundary conditions of the theory are obtained using the principle of variational calculus. From the formulated expression, the formula for calculation of the actual critical lateral imposed load, q𝑖𝑤, on the plate before deflection reaches the specified maximum specified limit and critical lateral imposed load, q𝑖𝑝, before plate reaches an elastic yield stress were obtained. By solving using the formulated expression, the effect of deflection and crack in a mild steel rectangular plates with opposite edge clamped and the other edge simply supported (CSCS) and simply supported at first and fourth edge and clamped at second edge and free of support at third edge (SCFS) were analysed and compared. This approach overcomes the challenges of the conventional practice in the structural analysis/design, which involves checking of deflection and shear; the process which is proved unreliable. In the result of CSCS plate, the positive value of the critical lateral imposed load, q𝑖𝑤(between 31.08735 N/mm to 155.4414 N/ mm) before deflection reaches the maximum specified limit and the critical lateral imposed load, q𝑖𝑝 (between 193.8246 N/mm to 193.8246 N/mm) before mild steel plate reaches the elastic yield stress, reveals that the plate neither failed in q𝑖𝑤 nor in q𝑖𝑝 for plate span (a) of 1000mm at allowable deflection, wa of 1mm to 5mm. Also, the positive value of critical lateral imposed load q𝑖𝑤 (between 16.23992 N/mm to 81.20424 N/mm) 𝑎𝑛𝑑 q𝑖𝑝(between 115.3523 N/ mm to 115.3523 N/mm) reveals that the plate neither fail in q𝑖𝑤 nor in q𝑖𝑝 for plate span (a) of 1000mm at allowable deflection, wa of 1mm to 5mm for SCFS. This means that the plate structure is safe. It is observed that the value of q𝑖𝑝 is constant at any value of wa for SCFS plate. This means that change in specified deflection limit does not affect the overall performance of SCFS rectangular plate unlike CSCS plate. Hence, it also reveals that the values of critical lateral imposed loads q𝑖𝑤 𝑎𝑛𝑑 q𝑖𝑝 decrease as the length-width ratio increases. This continues until failure occurs. This means that increase in plate width increases the chance of failure in a plate structure.It is concluded that the values of critical lateral load obtained by this theory gives realistic variation of transverse shear stress through the thickness of plate and satisfied the transverse flexibility of the rectangular plate’s condition while predicting the bending behaviour of isotropic thick rectangular plate. Therefore, using this theory it is possible to predict actual load that cause the bending behaviour of isotropic rectangular plate.


Author(s):  
W. L. Cleghorn ◽  
S. D. Yu

Abstract Reissner’s theory on shear-deformable plates is applied to analyze free flexural vibration of clamped rectangular plates. Accurate analytical solutions are obtained using the method of supeiposition. The first six eigenvalues with four digits of accuracy are presented for plates with three thickness ratios and six plate aspect ratios.


Sign in / Sign up

Export Citation Format

Share Document