Notch Sensitivity and Resistance to Tearing of Titanium Alloy Sheet

Notch Sensitivity and Resistance to Tearing of Titanium Alloy Sheet PDF Author: S. V. Arnold
Publisher:
ISBN:
Category :
Languages : en
Pages : 26

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Notch Sensitivity and Resistance to Tearing of Titanium Alloy Sheet

Notch Sensitivity and Resistance to Tearing of Titanium Alloy Sheet PDF Author: S. V. Arnold
Publisher:
ISBN:
Category :
Languages : en
Pages : 26

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Report on Notch Sensitivity of Titanium and Titanium Alloys

Report on Notch Sensitivity of Titanium and Titanium Alloys PDF Author: F. C. Holden
Publisher:
ISBN:
Category : Titanium
Languages : en
Pages : 104

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Sharp-Edge-Notch Tensile Characteristics of Several High-Strength Titanium Sheet Alloys at Room and Cryogenic Temperatures

Sharp-Edge-Notch Tensile Characteristics of Several High-Strength Titanium Sheet Alloys at Room and Cryogenic Temperatures PDF Author: G. B. Espey
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 34

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The 1-in. wide sharp edge notch tensile test was used to establish the notch sensitivity of several titanium sheet alloys including those of interest in the DOD Titanium Alloy Sheet Rolling Program. The influence of aging temperature was investigated in room-temperature tests and selected alloy conditions were also evaluated at -320 and -423 F. Room-temperature notch sensitivity develops with the aging reaction being most pronounced for the fully aged conditions and decreasing with overaging. A considerable reduction in notch sensitivity in some alloys can be obtained by overaging with relatively small loss in yield strength. At tensile strength to density ratios below about 1,000,000, the best ferritic steels known to the authors have notch sensitivities essentially equal to the poorest of the titanium alloys investigated. At higher strength to density values, the superiority of the titanium alloys rapidly increases. However, it should be noted that the strongest conditions of the titanium alloys possess fracture toughness, KC2, values sufficiently low that careful attention must be given to elimination of flaws in highly stressed components. At cryogenic temperatures, the titanium alloys exhibited higher notch sensitivity than alloys now normally employed for light weight cryogenic tankage. However, the -320 F and -423 F yield strength to density ratios of the commonly used materials are from 40 to 50 per cent lower than obtainable from titanium alloys. The elongation for several of the investigated titanium alloys exhibited a sharp drop between -320 F and -423 F. However, an equally sharp transition in the notch properties did not occur in this temperature range.

Nuclear Science Abstracts

Nuclear Science Abstracts PDF Author:
Publisher:
ISBN:
Category : Nuclear energy
Languages : en
Pages : 946

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Strain-rate Sensitivity of Three Titanium-alloy Sheet Materials After Prolonged Exposure at 550 ̊F (561 ̊K)

Strain-rate Sensitivity of Three Titanium-alloy Sheet Materials After Prolonged Exposure at 550 ̊F (561 ̊K) PDF Author: Robert M. Baucom
Publisher:
ISBN:
Category : Titanium alloys
Languages : en
Pages : 42

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U.S. Government Research Reports

U.S. Government Research Reports PDF Author:
Publisher:
ISBN:
Category : Science
Languages : en
Pages : 184

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Selected References on Brittle Fracture

Selected References on Brittle Fracture PDF Author: Don Owens
Publisher:
ISBN:
Category : Fracture mechanics
Languages : en
Pages : 68

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Interfaces in Composites

Interfaces in Composites PDF Author:
Publisher: ASTM International
ISBN:
Category :
Languages : en
Pages : 199

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Texture Strengthening and Fracture Toughness of Titanium Alloy Sheet at Room and Cryogenic Temperatures

Texture Strengthening and Fracture Toughness of Titanium Alloy Sheet at Room and Cryogenic Temperatures PDF Author: TL. Sullivan
Publisher:
ISBN:
Category : Biaxial stress
Languages : en
Pages : 12

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Biaxial yield strengths as high as 1.53 times uniaxial yield strength were obtained from burst tests of 6-in.-diameter cylindrical pressure vessels (1 to 2 stress field) fabricated from two textured titanium alloys, Ti-4Al-0.2O and Ti-5Al-2.5Sn ELI. Material nominally 0.020 in. thick was tested at 70, -320, and -423 F. While the Ti-4Al-0.2O alloy generally had superior biaxial smooth properties at the three test temperatures, the Ti-5Al-2.5Sn ELI alloy exhibited less notch sensitivity at-320 and -423 F. It is demonstrated that plastic Poisson's ratio obtained from a uniaxial test could be used to characterize the degree of texture in the two alloys and provide a means for predicting biaxial strengthening.

Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1126

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Book Description
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.