Please use this identifier to cite or link to this item: http://dspace.unimap.edu.my:80/xmlui/handle/123456789/35211
Title: J-integral analysis of surface cracks in round bars under combined loadings
Authors: A. Emran, Ismail
Ahmad Kamal, Ariffin
Shahrum, Abdullah
Mariyam Jameelah, Ghazali
Ruslizam, Daud, Dr.
emran@uthm.edu.my
kamal@eng.ukm.my
shahrum@eng.ukm.my
mariyam@eng.ukm.my
ruslizam@unimap.edu.my
Keywords: Finite element analysis
J-integral
Limit load
Stress intensity factor
Surface crack
Issue Date: Feb-2011
Publisher: Trans Tech Publications
Citation: Advanced Materials Research, vol. 214, 2011, pages 187-191
Abstract: This paper presents a non-linear numerical investigation of surface cracks in round bars under combined bending and torsion loadings by using ANSYS finite element analysis (FEA). Due to the non-symmetrical analysis, a full finite element (FE) model was constructed and special attention was given at the crack tip of the cracks. The surface cracks were characterized by the dimensionless crack aspect ratio, a/b = 0.6, 0.8, 1.0 and 1.2, while the dimensionless relative crack depth, a/D = 0.1, 0.2 and 0.3. The square-root singularity of stresses and strains was modeled by shifting the mid-point nodes to the quarter-point locations in the region around the crack front. The proposed model was validated with the existing model before any further analysis. The elastic-plastic analysis under the loading was assumed to follow the Ramberg-Osgood relation with strain hardening exponent, n = 5 and 10. J values were determined for all positions along the crack front and then, the limit load was predicted using the J values obtained from FEA through the reference stress method.
Description: Link to publisher's homepage at http://www.ttp.net/
URI: http://www.scientific.net/AMR.214.187
http://dspace.unimap.edu.my:80/dspace/handle/123456789/35211
ISSN: 1022-6680 (Print)
1662-8985 (Online)
Appears in Collections:Ruslizam Daud, Assoc Prof. Ir. Dr.



Items in UniMAP Library Digital Repository are protected by copyright, with all rights reserved, unless otherwise indicated.