Development of an Improved High Cycle Fatigue CriterionSource: Journal of Engineering for Gas Turbines and Power:;2007:;volume( 129 ):;issue: 001::page 162Author:Onome Scott-Emuakpor
,
Tommy George
,
Charles J. Cross
,
M.-H. Herman Shen
,
Jeffrey Calcaterra
DOI: 10.1115/1.2360599Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: An integrated computational-experimental approach for prediction of total fatigue life applied to a uniaxial stress state is developed. The approach consists of the following elements: (1) development of a vibration based fatigue testing procedure to achieve low cost bending fatigue experiments and (2) development of a life prediction and estimation implementation scheme for calculating effective fatigue cycles. A series of fully reversed bending fatigue tests were carried out using a vibration-based testing procedure to investigate the effects of bending stress on fatigue limit. The results indicate that the fatigue limit for 6061-T6 aluminum is approximately 20% higher than the respective limit in fully reversed tension-compression (axial). To validate the experimental observations and further evaluate the possibility of prediction of fatigue life, an improved high cycle fatigue criterion has been developed, which allows one to systematically determine the fatigue life based on the amount of energy loss per fatigue cycle. A comparison between the prediction and the experimental results was conducted and shows that the criterion is capable of providing accurate fatigue life prediction.
keyword(s): Fatigue , Stress , Compression , Cycles , Tension , Fatigue testing , Fatigue life , Aluminum , Fatigue limit AND Vibration ,
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contributor author | Onome Scott-Emuakpor | |
contributor author | Tommy George | |
contributor author | Charles J. Cross | |
contributor author | M.-H. Herman Shen | |
contributor author | Jeffrey Calcaterra | |
date accessioned | 2017-05-09T00:23:49Z | |
date available | 2017-05-09T00:23:49Z | |
date copyright | January, 2007 | |
date issued | 2007 | |
identifier issn | 1528-8919 | |
identifier other | JETPEZ-26935#162_1.pdf | |
identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/135783 | |
description abstract | An integrated computational-experimental approach for prediction of total fatigue life applied to a uniaxial stress state is developed. The approach consists of the following elements: (1) development of a vibration based fatigue testing procedure to achieve low cost bending fatigue experiments and (2) development of a life prediction and estimation implementation scheme for calculating effective fatigue cycles. A series of fully reversed bending fatigue tests were carried out using a vibration-based testing procedure to investigate the effects of bending stress on fatigue limit. The results indicate that the fatigue limit for 6061-T6 aluminum is approximately 20% higher than the respective limit in fully reversed tension-compression (axial). To validate the experimental observations and further evaluate the possibility of prediction of fatigue life, an improved high cycle fatigue criterion has been developed, which allows one to systematically determine the fatigue life based on the amount of energy loss per fatigue cycle. A comparison between the prediction and the experimental results was conducted and shows that the criterion is capable of providing accurate fatigue life prediction. | |
publisher | The American Society of Mechanical Engineers (ASME) | |
title | Development of an Improved High Cycle Fatigue Criterion | |
type | Journal Paper | |
journal volume | 129 | |
journal issue | 1 | |
journal title | Journal of Engineering for Gas Turbines and Power | |
identifier doi | 10.1115/1.2360599 | |
journal fristpage | 162 | |
journal lastpage | 169 | |
identifier eissn | 0742-4795 | |
keywords | Fatigue | |
keywords | Stress | |
keywords | Compression | |
keywords | Cycles | |
keywords | Tension | |
keywords | Fatigue testing | |
keywords | Fatigue life | |
keywords | Aluminum | |
keywords | Fatigue limit AND Vibration | |
tree | Journal of Engineering for Gas Turbines and Power:;2007:;volume( 129 ):;issue: 001 | |
contenttype | Fulltext |