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NASA-TM-X-3316

An investigation of fracture toughness, fatigue-crack growth, sustained-load flaw growth, and impact properties of three pressure vessel steels

Organization:
NASA - National Aeronautics and Space Administration (NASA)
Year: 1975

Abstract: The elastic fracture toughness of the three steels is shown to not decrease significantly with decreasing temperature from room temperature to about 244 K (-20 F.). The elastic fracture toughness of the three steels increased with increasing specimen width and thickness. The fatigue-crack-growth data for all three steels fall into relatively narrow scatter bands on plots of rate against stress-intensity range. An equation is shown to predict the upper bounds of the scatter bands reasonably well. Charpy impact energies decreased with decreasing temperature in the nominal temperature range from room temperature to 244 K (-20 F). The nil-ductility temperatures of the steels are discussed.
URI: https://yse.yabesh.ir/std/handle/yse/11316
Subject: CHARPY IMPACT TEST
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    NASA-TM-X-3316

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contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T15:12:47Z
date available2017-09-04T15:12:47Z
date copyright01/01/1975
date issued1975
identifier otherLYHOEEAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/11316
description abstractThe elastic fracture toughness of the three steels is shown to not decrease significantly with decreasing temperature from room temperature to about 244 K (-20 F.). The elastic fracture toughness of the three steels increased with increasing specimen width and thickness. The fatigue-crack-growth data for all three steels fall into relatively narrow scatter bands on plots of rate against stress-intensity range. An equation is shown to predict the upper bounds of the scatter bands reasonably well. Charpy impact energies decreased with decreasing temperature in the nominal temperature range from room temperature to 244 K (-20 F). The nil-ductility temperatures of the steels are discussed.
languageEnglish
titleNASA-TM-X-3316num
titleAn investigation of fracture toughness, fatigue-crack growth, sustained-load flaw growth, and impact properties of three pressure vessel steelsen
typestandard
page57
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1975
contenttypefulltext
subject keywordsCHARPY IMPACT TEST
subject keywordsCRACKING (FRACTURING)
subject keywordsDUCTILITY
subject keywordsFATIGUE (MATERIALS)
subject keywordsFRACTURE STRENGTH
subject keywordsIMPACT LOADS
subject keywordsPRESSURE VESSELS
subject keywordsSTEELS
subject keywordsSTRESS ANALYSIS
subject keywordsTABLES (DATA)
subject keywordsTEMPERATURE EFFECTS
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