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contributor authorHoward A. Canistraro
contributor authorEric H. Jordan
contributor authorLeroy H. Favrow
contributor authorFrancis A. Reed
contributor authorShi Shixiang
date accessioned2017-05-08T23:56:45Z
date available2017-05-08T23:56:45Z
date copyrightJuly, 1998
date issued1998
identifier issn0094-4289
identifier otherJEMTA8-26992#242_1.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/120519
description abstractAn acoustic time of flight technique is described in detail for measuring the elastic constants of cubic single crystals that allows for the constants to be determined at elevated temperature. Although the overall technique is not new, various aspects of the present work may prove extremely useful to othersinterested in finding these values, especially for aerospace materials applications. Elastic constants were determined for the nickel based alloy, Hastelloy X from room temperature to 1000°C. Accurate elastic constants were needed as part of an effort to predict both polycrystal mechanical properties and the nature of grain induced heterogeneous mechanical response. The increased accuracy of the acoustically determined constants resulted in up to a 15 percent change in the predicted stresses in individual grains. These results indicate that the use of elastic single crystal constants of pure nickel as an approximation for the constants of gas turbine single crystal alloys, which is often done today, is inaccurate.
publisherThe American Society of Mechanical Engineers (ASME)
titleElastic Constants of Single Crystal Hastelloy X at Elevated Temperatures
typeJournal Paper
journal volume120
journal issue3
journal titleJournal of Engineering Materials and Technology
identifier doi10.1115/1.2812350
journal fristpage242
journal lastpage247
identifier eissn1528-8889
keywordsTemperature
keywordsCrystals
keywordsElastic constants
keywordsNickel
keywordsAlloys
keywordsAcoustics
keywordsStress
keywordsMechanical properties
keywordsAerospace industry
keywordsGas turbines
keywordsApproximation AND Flight
treeJournal of Engineering Materials and Technology:;1998:;volume( 120 ):;issue: 003
contenttypeFulltext


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