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contributor authorM. D. Rowe
contributor authorV. R. Ishwar
contributor authorD. L. Klarstrom
date accessioned2017-05-09T00:19:52Z
date available2017-05-09T00:19:52Z
date copyrightApril, 2006
date issued2006
identifier issn1528-8919
identifier otherJETPEZ-26905#354_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/133695
description abstractAlloy selection and alloy design both require consideration of an array of material attributes, including in-service properties, weldability, and fabricability. Critical properties of modern heat-resistant alloys for gas turbine applications include high-temperature strength, thermal stability, oxidation resistance, and fatigue resistance. In this paper, the properties of 12 solid-solution-strengthened and six age-hardenable heat-resistant alloys are compared. Weldability is an important attribute and can be a major limiting factor in the use of certain alloys. Weldability test methods are discussed, and the resistance of alloys to solidification cracking and strain-age cracking is compared. The use of weldability testing in the development of modern heat-resistant alloys is discussed with several examples cited. Finally, alloy selection for gas turbine components is outlined, taking into account both alloy properties and fabricability.
publisherThe American Society of Mechanical Engineers (ASME)
titleProperties, Weldability, and Applications of Modern Wrought Heat-Resistant Alloys for Aerospace and Power Generation Industries
typeJournal Paper
journal volume128
journal issue2
journal titleJournal of Engineering for Gas Turbines and Power
identifier doi10.1115/1.2056527
journal fristpage354
journal lastpage361
identifier eissn0742-4795
keywordsAlloys
keywordsFracture (Process)
keywordsHeat AND Electrical resistance
treeJournal of Engineering for Gas Turbines and Power:;2006:;volume( 128 ):;issue: 002
contenttypeFulltext


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