Unequivocally Nonconservative Results From One Method of Imperfection Quantification in RCC-MR

2020 ◽  
Vol 7 (1) ◽  
Author(s):  
Ashok Kumar ◽  
Anindya Chatterjee

Abstract Design against buckling of thin shells at high temperatures often follows the code RCC-MR. RCC-MR allows three methods to quantify shell imperfections for use in safe load calculations, where lower imperfection values raise the safe load estimates. In recent work, we showed that the third of these methods can sometimes yield remarkably low imperfection values, leading to potentially nonconservative designs, but nonconservatism of the method was not proved. Here, we prove nonconservatism in two designs based on the third method. Proving such nonconservatism is difficult using experiments or with large material nonlinearity in simulations. We first discuss these difficulties to motivate our approach. We then present two examples: a spherical shell and a torispherical shell, both under external pressure. The shell walls are thin enough so that plasticity is not encountered before structural collapse. For specific shape imperfections, we show with geometrically nonlinear, purely elastic, highly refined, post-buckling analysis using abaqus that the physical loads at which the imperfect shells collapse are overpredicted via RCC-MR's third method by factors of about 8/7 and 11/10, respectively. We emphasize that code-based design using nonlinear simulation prescribes a further safety factor of 2.5, which we have denied ourselves here in order to give the third method the benefit of doubt. We conclude that the third imperfection quantification method in RCC-MR should be reexamined.

2019 ◽  
Vol 5 (4) ◽  
Author(s):  
Ashok Kumar ◽  
Anindya Chatterjee

The thin shell design code RCC-MR is used for sodium-cooled fast breeder reactor components operating at high temperatures. Thin shells from such applications can be designed using linear elastic buckling analysis, following procedures given in RCC-MR. For human safety, such procedures can and should be examined by the broader scientific community. Among such procedures, RCC-MR provides three alternative methods to quantify an imperfection value; and that value is used in subsequent calculations to determine safe loads. Of these methods, the third seems potentially nonconservative for some situations. Here, we examine that third method using detailed numerical examples. These examples, found by trial and error, are the main contribution of this paper. The first example is a nonuniform cylindrical shell closed with a spherical endcap under external pressure. The second is a cylinder with an ellipsoidal head under internal pressure. The third is an L-shaped pipe with an end load. In all three cases, the new computed imperfection quantity is found to be surprisingly small compared to the actual value used for computations (e.g., 25 times smaller), and in two cases, the result is insensitive to the actual imperfection. We explain how the three examples “trick” the imperfection quantification method in three different ways. We suggest that this imperfection quantification method in RCC-MR should be re-examined. The primary value of our paper lies not in new mechanics, but in identifying unexpected ways in which a particular step in shell design using RCC-MR could be potentially nonconservative.


PAMM ◽  
2019 ◽  
Vol 19 (1) ◽  
Author(s):  
Mehran Motevalli ◽  
Daniel Balzani ◽  
Jörg Uhlemann ◽  
Natalie Stranghöner

2016 ◽  
Vol 2016 (0) ◽  
pp. G0300706
Author(s):  
Kazuyuki TSUKIMORI ◽  
Hiroki YADA ◽  
Masanori ANDO ◽  
Masakazu ICHIMIYA ◽  
Yoshinari ANODA ◽  
...  

1988 ◽  
Vol 55 (1) ◽  
pp. 136-142 ◽  
Author(s):  
G. Sun ◽  
J. S. Hansen

Optimization of the buckling load of a laminated-composite, circular-cylindrical shell subjected to axial compression, external pressure, torsion, or a combination thereof is undertaken. In the optimization procedure it is assumed that the shell has a fixed weight (length, radius and thickness); the buckling load is taken as the objective function which is maximized by adopting the lamina fiber orientations as the optimizing parameters. For the shell analysis a perturbation approach is used and the boundary conditions and nonlinear prebuckling effects are included; the analysis yields both the buckling load and the post-buckling character of the shell. The procedure developed is demonstrated for eight loading configurations. In addition, selected laminates were chosen for an experimental programme involving a series of graphite/epoxy shells. The predicted analytical and the measured experimental buckling loads are in very good agreement.


1990 ◽  
Vol 57 (4) ◽  
pp. 989-994 ◽  
Author(s):  
Herzl Chai

The large-deflection plate solution developed in Part I is used here to study the buckling and post-buckling deformation and stress characteristics of an elliptically-shaped surface layer that has been delaminated from a large material body. The economical, yet accurate nature of this solution, together with available graphic routines, has made it possible to present, figuratively, a comprehensive description of the plate behavior. The conditions for a layer-substrate overlap and the variations of membrane and bending stresses along the plate boundary are emphasized. Deformations were induced either by a normal pressure or a biaxial displacement field applied to the plate boundary. The problem variables are plate size and shape, details of load biaxiality, and load level.


1989 ◽  
Vol 4 (4) ◽  
pp. 193-217 ◽  
Author(s):  
C. Borri ◽  
S. Chiostrini

In the context of a nonlinear stability theory of elastic structures, the geometrically nonlinear formulation of a spatial beam element (recently introduced by several authors) is reviewed for application to a perturbative approach of the post-buckling analysis of space beam grids or frames. The implementation aspects of the procedure in an iterative-incremental algorithm are discussed, and the performances of several implemented iteration strategies are brought out, with the aim of improving the usual known ones. The adopted strategy to detect and trace post-buckling equilibrium paths is then discussed. Finally, some numerical examples are used to demonstrate the characteristics and capabilities of the analytical model.


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