On the Continuance of an Analytical Solution across the Elastic-Plastic Boundary of a Mode I Fracture Mechanics Problem

Author(s):  
David J. Unger
1994 ◽  
Vol 23 (1) ◽  
pp. 1-11 ◽  
Author(s):  
P. Rathinam ◽  
R. Narayanan ◽  
G. Jayarama Rao

Author(s):  
Phuong H. Hoang ◽  
Douglas A. Scarth

Tabulation solution for ductile tearing failure of piping axial flaws was first implemented in the A90 Addendum to the 1989 Edition of the ASME B&PV, Section XI, Appendix H. The solution was based on J-Tearing analyses of pipe axial semi-elliptical part-through wall flaws in a generic ferritic material that has J1C > = 600 in-lbs/in2. Analytical solution for pipe axial flaw has not been implemented in the Code. In this paper a general load multiflier Z-factor is developed for use in an analytical solution for pipe axial part-through wall flaw, which is compatible with the current Elastic-Plastic Fracture Mechanics (EPFM) tabular solution in the Section XI, Appendix C. The Z-curve is developed using the same J-Tearing analysis technique and the same generic material properties for ferritic materials that were used in the development of the Code tabulation solutions. The predicted failure stresses using the Z curve are fairly corelated and conservatively the actual failure stress in the available test specimens from the PIFRAC database.


2000 ◽  
Author(s):  
Leishan Chen ◽  
Peter Ifju ◽  
Bhavani Sankar

2019 ◽  
Vol 135 (5) ◽  
pp. 33-41 ◽  
Author(s):  
Minami KATAOKA ◽  
Yuzo OBARA ◽  
Leona VAVRO ◽  
Kamil SOUCEK ◽  
Sang-Ho CHO ◽  
...  

2020 ◽  
Vol 8 (1) ◽  
Author(s):  
Jyotikalpa Bora ◽  
Sushen Kirtania

Abstract A comparative study of elastic properties and mode I fracture energy has been presented between conventional carbon fibre (CF)/epoxy and advanced carbon nanotube (CNT)/epoxy laminated composite materials. The volume fraction of CNT fibres has been considered as 15%, 30%, and 60% whereas; the volume fraction of CF has been kept constant at 60%. Three stacking sequences of the laminates viz.[0/0/0/0], [0/90/0/90] and [0/30/–30/90] have been considered in the present analysis. Periodic microstructure model has been used to calculate the elastic properties of the laminated composites. It has been observed analytically that the addition of only 15% CNT in epoxy will give almost the same value of longitudinal Young’s modulus as compared to the addition of 60% CF in epoxy. Finite element (FE) analysis of double cantilever beam specimens made from laminated composite has also been performed. It has been observed from FE analysis that the addition of 15% CNT in epoxy will also give almost the same value of mode I fracture energy as compared to the addition of 60% CF in epoxy. The value of mode I fracture energy for [0/0/0/0] laminated composite is two times higher than the other two types of laminated composites.


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