Fatigue life and crack growth analysis of keyhole specimen

This report deals with the prediction of fatigue life and crack growth for keyhole specimen using variable loading amplitude. The objective of this report is to predict the fatigue life and crack growth of keyhole specimen. The steel such as MANTEN and RQC100 were considered the keyhole materials. T...

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Main Author: Fua, Wai Loon
Format: Undergraduates Project Papers
Language:English
English
English
English
Published: 2010
Subjects:
Online Access:http://umpir.ump.edu.my/id/eprint/1791/
http://umpir.ump.edu.my/id/eprint/1791/
http://umpir.ump.edu.my/id/eprint/1791/1/Fatigue%20life%20and%20crack%20growth%20analysis%20of%20keyhole%20specimen%20%28Table%20of%20content%29.pdf
http://umpir.ump.edu.my/id/eprint/1791/2/Fatigue%20life%20and%20crack%20growth%20analysis%20of%20keyhole%20specimen%20%28Abstract%29.pdf
http://umpir.ump.edu.my/id/eprint/1791/3/Fatigue%20life%20and%20crack%20growth%20analysis%20of%20keyhole%20specimen%20%28Chapter%201%29.pdf
http://umpir.ump.edu.my/id/eprint/1791/4/Fatigue%20life%20and%20crack%20growth%20analysis%20of%20keyhole%20specimen%20%28References%29.pdf
id ump-1791
recordtype eprints
spelling ump-17912017-04-06T03:48:10Z http://umpir.ump.edu.my/id/eprint/1791/ Fatigue life and crack growth analysis of keyhole specimen Fua, Wai Loon TA Engineering (General). Civil engineering (General) This report deals with the prediction of fatigue life and crack growth for keyhole specimen using variable loading amplitude. The objective of this report is to predict the fatigue life and crack growth of keyhole specimen. The steel such as MANTEN and RQC100 were considered the keyhole materials. The structural three-dimensional solid modeling of keyhole specimen was developed using Solid work. The finite element model and analysis were performed using PATRAN and NASTRAN software. Predicted result is validated with existing experimental result. In addition, the fatigue life was predicted using the strain-life approach subjected to variable amplitude loading. From the results, it is observed that SAETRN loading gives the most conservative results for strain-life method. It is concluded that SAETRN loading history is the most conservative method compared to SAESUS and SAEBKT loading history. RQC100 has a longer crack initiation life but shorter crack propagation life than MANTEN. Apparently, MANTEN more ductile than RQC100. The RQC100 is suitable material of keyhole. 2010-12 Undergraduates Project Papers NonPeerReviewed application/pdf en http://umpir.ump.edu.my/id/eprint/1791/1/Fatigue%20life%20and%20crack%20growth%20analysis%20of%20keyhole%20specimen%20%28Table%20of%20content%29.pdf application/pdf en http://umpir.ump.edu.my/id/eprint/1791/2/Fatigue%20life%20and%20crack%20growth%20analysis%20of%20keyhole%20specimen%20%28Abstract%29.pdf application/pdf en http://umpir.ump.edu.my/id/eprint/1791/3/Fatigue%20life%20and%20crack%20growth%20analysis%20of%20keyhole%20specimen%20%28Chapter%201%29.pdf application/pdf en http://umpir.ump.edu.my/id/eprint/1791/4/Fatigue%20life%20and%20crack%20growth%20analysis%20of%20keyhole%20specimen%20%28References%29.pdf Fua, Wai Loon (2010) Fatigue life and crack growth analysis of keyhole specimen. Faculty of Mechanical Engineering, Universiti Malaysia Pahang. http://iportal.ump.edu.my/lib/item?id=chamo:52261&theme=UMP2
repository_type Digital Repository
institution_category Local University
institution Universiti Malaysia Pahang
building UMP Institutional Repository
collection Online Access
language English
English
English
English
topic TA Engineering (General). Civil engineering (General)
spellingShingle TA Engineering (General). Civil engineering (General)
Fua, Wai Loon
Fatigue life and crack growth analysis of keyhole specimen
description This report deals with the prediction of fatigue life and crack growth for keyhole specimen using variable loading amplitude. The objective of this report is to predict the fatigue life and crack growth of keyhole specimen. The steel such as MANTEN and RQC100 were considered the keyhole materials. The structural three-dimensional solid modeling of keyhole specimen was developed using Solid work. The finite element model and analysis were performed using PATRAN and NASTRAN software. Predicted result is validated with existing experimental result. In addition, the fatigue life was predicted using the strain-life approach subjected to variable amplitude loading. From the results, it is observed that SAETRN loading gives the most conservative results for strain-life method. It is concluded that SAETRN loading history is the most conservative method compared to SAESUS and SAEBKT loading history. RQC100 has a longer crack initiation life but shorter crack propagation life than MANTEN. Apparently, MANTEN more ductile than RQC100. The RQC100 is suitable material of keyhole.
format Undergraduates Project Papers
author Fua, Wai Loon
author_facet Fua, Wai Loon
author_sort Fua, Wai Loon
title Fatigue life and crack growth analysis of keyhole specimen
title_short Fatigue life and crack growth analysis of keyhole specimen
title_full Fatigue life and crack growth analysis of keyhole specimen
title_fullStr Fatigue life and crack growth analysis of keyhole specimen
title_full_unstemmed Fatigue life and crack growth analysis of keyhole specimen
title_sort fatigue life and crack growth analysis of keyhole specimen
publishDate 2010
url http://umpir.ump.edu.my/id/eprint/1791/
http://umpir.ump.edu.my/id/eprint/1791/
http://umpir.ump.edu.my/id/eprint/1791/1/Fatigue%20life%20and%20crack%20growth%20analysis%20of%20keyhole%20specimen%20%28Table%20of%20content%29.pdf
http://umpir.ump.edu.my/id/eprint/1791/2/Fatigue%20life%20and%20crack%20growth%20analysis%20of%20keyhole%20specimen%20%28Abstract%29.pdf
http://umpir.ump.edu.my/id/eprint/1791/3/Fatigue%20life%20and%20crack%20growth%20analysis%20of%20keyhole%20specimen%20%28Chapter%201%29.pdf
http://umpir.ump.edu.my/id/eprint/1791/4/Fatigue%20life%20and%20crack%20growth%20analysis%20of%20keyhole%20specimen%20%28References%29.pdf
first_indexed 2023-09-18T21:55:02Z
last_indexed 2023-09-18T21:55:02Z
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