Stress Intensity Factor of Notch/Crack Configuration under Bending Load for Brittle Materials

Author(s):  
Feng Hui Wang
2006 ◽  
Vol 324-325 ◽  
pp. 1051-1054
Author(s):  
Feng Hui Wang

Stress intensity factor of crack ahead of notch is important for understanding the failure of this kind structure. In this paper, a model is proposed to calculate the stress intensity factor of crack ahead notch configuration under bending load, the modeling value were verified by the data from literatures and experimental data of this paper, the trend of the value from model is agreement with that from experiments.


2017 ◽  
Vol 909 ◽  
pp. 133-142
Author(s):  
Teng Hui Chen

Sharp V-notches with various angles often appear in engineering structures. When being loaded, the high stress at the apex could result in crack propagation on the structure and further fracture. For this reason, safety evaluation should be emphasized for products or engineering structures with such geometric characteristics. Sharp V-notches are regarded as wedge structures that the above situations seriously and often appear on brittle materials. Regarding the stress intensity factor K of the driving force for wedge structure failure, Chen, Dunn, and Seweryn, with numerical analysis for the fracture experiment, explained that the critical stress intensity factor Kc for single isotropic material fracture could be the intensity failure specification for wedge structures. Nevertheless, V-notched brittle materials are likely to receive great stress over the surface elastic energy of the structure when being loaded, causing brittle failure at the apex. When the high-strength and light-weight composite material is attached to reinforce the surface of brittle materials, the energy is reinforced to enhance the critical stress intensity factor of the overall structure, aiming to improve the failure of brittle materials resulted from stress singularity. This paper therefore tends to discuss the effects of the composite attachment, layer, and fiber reinforced direction on the critical stress intensity factor when the structure is being fractured.


2010 ◽  
Vol 2010 (0) ◽  
pp. 1016-1018
Author(s):  
Kiyotaka MASAKI ◽  
Fumiya KUWAE ◽  
Yuji SANO ◽  
Masayuki KAMAYA ◽  
Kentaro KAJIWARA

2020 ◽  
Vol 10 (12) ◽  
pp. 4142
Author(s):  
Gong Hai ◽  
Yi Bin ◽  
Wu Yunxin ◽  
Liao Zhiqi ◽  
Liu Yaoqiong ◽  
...  

The finite element model of integral wing panels with central penetration cracks under bending load was established, and the crack propagation process of the aircraft panel was simulated. The stress intensity factor (SIF) of the crack tip during crack propagation under varying conditions of crack length and panel structural parameters was determined. The effects of the panel structure parameters and crack size on the crack tip SIF were obtained. The regression analysis of the finite simulation element results has been performed and a regression model of SIF at the crack tip of the integral panel has been established, the determination coefficient of the regression model is 0.955.


2005 ◽  
Vol 20 (2) ◽  
pp. 83-90 ◽  
Author(s):  
Y. B. Shao

Stress intensity factor (SIF) is frequently used by designers to predict the integrity and residual life of a tubular joint containing a surface crack. In this study, a new numerical modelling method for cracked tubular K-joints has been presented. The proposed model has been verified from experimental results to be accurate and reliable in evaluation of the stress intensity factor for any tubular K-joint with a surface crack. Thereafter, parametric study for more than five thousand numerical models of tubular K-joints with a surface crack subjected to balanced in-plane bending load (IPB) has been carried out. A parametric equation to estimate the SIF value of any cracked tubular K-joint under IPB is then proposed based on the computed numerical results. Error analysis has been also carried out and it shows that the proposed equation can provide reliable and accurate estimation of the SIF value for cracked tubular K-joints under IPB.


2014 ◽  
Vol 6 ◽  
pp. 586472 ◽  
Author(s):  
Tielin Chen ◽  
Chao Li ◽  
Dingli Zhang

A numerical approach to simulate the crack initiation and propagation process of the nonlinear fracture behavior of the quasi-brittle materials under tensile loading is presented. The nonlinear fracture of Mode I of quasi-brittle material is analyzed by considering the effects of microscopic softening rate and heterogeneity. The results show that the softening rate and the heterogeneity of quasi-brittle material affect the values of stress intensity factor K I. The softening index affects merely the size of the plastic zones while the heterogeneity causes the more sophisticated response of quasi-brittle materials.


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