Crack arrest in Si3N4-based layered composites with residual stress

2004 ◽  
Vol 64 (13-14) ◽  
pp. 1947-1957 ◽  
Author(s):  
M. Lugovy ◽  
V. Slyunyayev ◽  
V. Subbotin ◽  
N. Orlovskaya ◽  
G. Gogotsi
1991 ◽  
Vol 113 (3) ◽  
pp. 380-384
Author(s):  
P. B. Crosley ◽  
E. J. Ripling

Safety of structures can be assured, even if cracks initiate in localized regions of abnormally low toughness, and/or abnormally high stress (LT/HS), if the materials from which they are fabricated have a high enough crack arrest fracture toughness. When this requirement is met, fast-running cracks that initiate in LT/HS regions arrest when their tip encounters material having normal toughness and stresses. The work described in this paper was carried out to determine the crack arrest capability of LNG storage tanks by determining the longest LT/HS region in which a crack could initiate and still arrest when it leaves this region. The determination consisted of relating a fracture analysis with the measured full-thickness crack arrest fracture toughness of three 9-percent Ni plates which were reported in reference [1]. The calculations used a residual stress pattern, produced by welding, superimposed on a typical membrane stress. The residual stress was selected as an example of a localized high stress region. It was found that tanks built from the poorest of the three tested plates could arrest cracks about 3/4 m long, while tanks built from the two tougher plates could arrest cracks almost 2 m long.


2020 ◽  
Vol 64 (7) ◽  
pp. 1161-1174
Author(s):  
Chiyomi Iwatake ◽  
Masahito Kaneko ◽  
Kazuyuki Matsumoto ◽  
Tsutomu Fukui ◽  
Shuji Aihara ◽  
...  

1997 ◽  
Vol 12 (9) ◽  
pp. 2357-2365 ◽  
Author(s):  
Jow-Lay Huang ◽  
Feng-Chi Chou ◽  
Horng-Hwa Lu

The present study involved the fabrication of three-layered composites consisting of outer layers that contained Si3N4 and an inner layer that contained TiN in a Si3N4 matrix. Surface compressive stresses were developed upon cooling due to the relatively higher thermal expansion coefficient (CTE) in the inner layer. The flexural strength of layered Si3N4 composites was substantially greater than that of monolithic Si3N4. This was attributed to the surface compressive stress. The effects of TiN composition and inner layer thickness on the mechanical properties were investigated. Layered samples containing 20 vol.% TiN had lower flexural strength than Si3N4–10% TiN/Si3N4–Si3N4 due to the formation of microcracks in the inner layer. Crack behaviors in layered samples were affected by the residual stress, interface, and free sample surface. Both theoretical and experimental results indicated that the strength and toughness of layered composites were substantially greater than those of monolithic materials. The determination of fracture toughness in three-layered materials by the surface indentation technique should be done carefully due to the influence of residual stress.


2006 ◽  
Vol 11-12 ◽  
pp. 77-80
Author(s):  
Seog Young Yoon ◽  
Ron Stevens ◽  
Hong Chae Park

Symmetric three-layer alumina/zirconia/mullite composites have been prepared by tape casting and hot-pressing (20 MPa) at 1500°C for 2 h in argon. The hardness and Young’s modulus of the layered materials were evaluated using low load continuous depth-sensing indentation equipment (nanoindentation), appear to be affected by the formation of processing defects and residual stress.


2009 ◽  
Vol 1242 ◽  
Author(s):  
G. Urriolagoitia-Sosa ◽  
A. Molina-Ballinas ◽  
G. Urriolagoitia-Calderón ◽  
L. H. Hernández-Gómez ◽  
y J. M. Sandoval-Pineda

ABSTRACTFor centuries, the manipulation of mechanical properties for the development of components has been extremely important. Its relevance is based on improving the service life in the components. The aim of some techniques that have been used is to introduce strain hardening (tensile) and a beneficial residual stress field. Nevertheless, the application of both methods is very common when the component is manufactured, but the lack of knowledge of the final physical state of the material could compromise the structural integrity of the final product. This work presents a numerical evaluation concerning the characterization of a stainless steel AISI 316L, having a homogeneous axial history and a residual stress field. The relevance of the work is focused in a new methodology that can be used to improve the mechanical resistance of the component and to arrest crack propagation. By altering the mechanical properties of the material, it could be possible to delay nucleation and interrupt the propagation of cracks. This study also shows that if the strain hardening behaviour and the introduction of the residual stress field is not done properly, it could result in a component susceptible to fail. In the same sense, bending tests are proposed to provide tensile and compressive stress profiles.


1994 ◽  
Vol 28 (8) ◽  
pp. 684-707 ◽  
Author(s):  
H. Wang ◽  
T. Vu-Khanh

Low-velocity impact in carbon fiber/PEEK crossply laminates has been studied by test and analysis. Emphases of the study were focused on the material properties which may control the damage extension of transverse crack and delamination. It was found that, considering the thermal residual stress and the crack constraining effect, extension of transverse cracks could not be predicted by the Strength of Materials approach. The impact-induced delamination could be characterized by the crack arrest concept of fracture mechanics. The delamination resulted from a Mode II-dominated unstable fracture, which occurred under displacement-controlled conditions and seemed to be arrested at a constant interlaminar fracture energy. It was found that the thermoplastic APC-2 composite exhibits the same damage modes as epoxy composites under low velocity impact. Both the matrix-controlled damage and the fiber-controlled penetration may become the dominant failure mode, depending on the stacking sequence of the laminate. The residual stress in the thermoplastic laminates is as high as half of the transverse strength of the unidirectional material. The crack constraining effect tends to increase the in situ transverse strength of the lamina as the lamina thickness decreases. Considering the residual stress and crack constraining effect, the transverse crack extension cannot be predicted by the Strength of Materials approach. The crack arrest concept of fracture mechanics seems to be a useful approach to predict the extension of impact-induced delamination. The delamination resulted from a Mode II-dominated unstable fracture, which occurred under displacement-controlled conditions and seemed to be arrested at a constant interlaminar fracture energy. By assuming the delamination arrest at about the time of maximum impact load, the delamination arrest toughness could be evaluated from the test data of [05/905/05] laminates. The delamination arrest toughness is also found to be close to the Mode II-propagation toughness of the material.


2008 ◽  
Vol 368-372 ◽  
pp. 1803-1806
Author(s):  
Dae Suk Han ◽  
Chi Seung Lee ◽  
Min Sung Chun ◽  
Myung Hyun Kim ◽  
Hong Chae Park ◽  
...  

For enhanced mechanical properties of ceramics for structural application, a great deal of attention has concentrated on preparation of layered composites. In this study, numerical simulation technique, which is applicable for the evaluation of mechanical performance for layered composite material, was developed. A generalized material constitutive equation coupled with material damage model based on the continuum damage mechanics approach was proposed and has been implemented to an in-house type finite element analysis code. The material behaviors for each component of layered composites can be simulated by the pre-defined material model on the simulation. A series of finite element analyses was carried out in order to elucidate the effect of fabrication related residual stress on the structural capacity of the layered composites.


2018 ◽  
Vol 668 ◽  
pp. 14-22 ◽  
Author(s):  
D. Kozic ◽  
H.-P. Gänser ◽  
R. Brunner ◽  
D. Kiener ◽  
T. Antretter ◽  
...  

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