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  • MATERIALS, METALLIC  (5)
  • AIRCRAFT DESIGN, TESTING AND PERFORMANCE
  • 1970-1974  (5)
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  • 1
    Publication Date: 2019-06-27
    Description: The effects on fracture and flaw growth of weld-induced residual stresses, combined bending and tension stresses, and stress fields adjacent to circular holes in 2219-T87 aluminum and 5AI-2.5Sn(ELI) titanium alloys were evaluated. Static fracture tests were conducted in liquid nitrogen; fatigue tests were performed in room air, liquid nitrogen, and liquid hydrogen. Evaluation of results was based on linear elastic fracture mechanics concepts and was directed to improving existing methods of estimating minimum fracture strength and fatigue lives for pressurized structure in spacecraft and booster systems. Effects of specimen design in plane-strain fracture toughness testing were investigated. Four different specimen types were tested in room air, liquid nitrogen and liquid hydrogen environments using the aluminum and titanium alloys. Interferometry and holograph were used to measure crack-opening displacements in surface-flawed plexiglass test specimens. Comparisons were made between stress intensities calculated using displacement measurements, and approximate analytical solutions.
    Keywords: MATERIALS, METALLIC
    Type: NASA-CR-72659
    Format: application/pdf
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  • 2
    Publication Date: 2019-06-27
    Description: Electrical resistivity measurements on pure metals in temperature range 0 to 273 K
    Keywords: MATERIALS, METALLIC
    Type: NASA-CR-113877 , NBS-TN-365-1
    Format: application/pdf
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  • 3
    Publication Date: 2019-07-13
    Description: The combined effects of weld-induced residual stresses and flaws on fracture strength were experimentally evaluated by testing Ti-5Al-2.5Sn surface flawed specimens at -320F (-195C) in liquid nitrogen. Flaws were located in weld metal with crack planes either parallel to or perpendicular to gas tungsten arc weld centerlines, and in base metal with the crack plane perpendicular to the rolling direction. Tests were conducted using two different flaw sizes to effect fracture stresses at two different levels including one level either at or near, and one level well below the tensile yield strength. Three different residual stress levels were generated, measured, and tested. Results were evaluated using modified linear elastic fracture mechanics theory.
    Keywords: MATERIALS, METALLIC
    Type: Meeting on Significance of Defects in Welded Structures; Oct 15, 1973 - Oct 19, 1973; Tokyo; Japan
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  • 4
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    Unknown
    In:  Other Sources
    Publication Date: 2019-07-13
    Description: Surface strain cyclic flaw growth rates for Al and Ti plates, using end point, flaw opening and striation measurements
    Keywords: MATERIALS, METALLIC
    Type: ; 23-26, 28, 30 (|NATIONAL SYMPOSIUM ON FRACTURE MECHANICS; Aug 25, 1969 - Aug 27, 1969; BETHLEHEM, PA
    Format: text
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  • 5
    Publication Date: 2019-07-13
    Description: Specimen design effects on Al and Ti alloy plane strain fracture toughness at room and cryogenic temperatures, discussing crack propagation and rolling directions orientations
    Keywords: MATERIALS, METALLIC
    Type: ANNUAL MEETING ON FRACTURE TOUGHNESS TESTING AT CRYOGENIC TEMPERATURES; Jun 21, 1970 - Jun 26, 1970; TORONTO; CANADA
    Format: text
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