Show simple item record

contributor authorT. H. Krukemyer
contributor authorR. W. Swindeman
contributor authorA. Fatemi
date accessioned2017-05-08T23:44:28Z
date available2017-05-08T23:44:28Z
date copyrightJanuary, 1994
date issued1994
identifier issn0094-4289
identifier otherJEMTA8-26961#54_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/113725
description abstractAn experimental investigation was conducted on Haynes Alloy 556 to study the fatigue behavior of the material at elevated temperatures. Fatigue tests were run at constant temperatures ranging from room temperature to 871°C with strain ranges from 0.265 to 1.5 percent resulting in lives between 102 and 106 cycles. Cyclic deformation properties were evaluated based on the fatigue data. Three fatigue life models were evaluated for their ability to predict the isothermal fatigue lives of the material. These included the Ostergren, Frequency Separation and Stress-Strain-Time models. Strengths and weaknesses of each model are discussed based on the experimental results.
publisherThe American Society of Mechanical Engineers (ASME)
titleFatigue Behavior of a 22Cr-20Ni-18Co-Fe Alloy at Elevated Temperatures
typeJournal Paper
journal volume116
journal issue1
journal titleJournal of Engineering Materials and Technology
identifier doi10.1115/1.2904255
journal fristpage54
journal lastpage61
identifier eissn1528-8889
keywordsAlloys
keywordsFatigue
keywordsTemperature
keywordsSeparation (Technology)
keywordsDeformation
keywordsStress
keywordsCycles
keywordsFatigue life AND Fatigue testing
treeJournal of Engineering Materials and Technology:;1994:;volume( 116 ):;issue: 001
contenttypeFulltext


Files in this item

Thumbnail

This item appears in the following Collection(s)

Show simple item record