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  • 1970-1974  (4)
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  • 1
    Publication Date: 2019-06-27
    Description: The miniature Izod and Charpy impact strengths of copper, copper-nickel, and nickel-base superalloy uniaxially reinforced with continuous tungsten fibers were studied. In most cases, impact strength was increased by increasing fiber or matrix toughness, decreasing fibermatrix reaction, increasing test temperature, hot working, or heat treating. Notch sensitivity was reduced by increasing fiber content or matrix toughness. An equation relating impact strength to fiber and matrix properties and fiber content was developed. Program results imply that tungsten alloy-fiber/superalloy matrix composites can be made with adequate impact resistance for turbine blade or vane applications.
    Keywords: MATERIALS, METALLIC
    Type: NASA-TN-D-7393 , E-5857
    Format: application/pdf
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  • 2
    Publication Date: 2019-06-27
    Description: Impact properties determined for pure copper, copper-nickel alloy, and superalloy metal matrix composites reinforced with tungsten fibers
    Keywords: MATERIALS, NONMETALLIC
    Type: NASA-TM-X-67810
    Format: application/pdf
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  • 3
    Publication Date: 2019-07-13
    Description: Impact strength of Cu, Cu-Ni alloy and superalloy matrices reinforced with W fibers, studying temperature, heat treatment and fiber content and toughness effects
    Keywords: MATERIALS, METALLIC
    Type: ANNUAL CONFERENCE ON COMPOSITE MATERIALS- TESTING AND DESIGN; Apr 20, 1971 - Apr 22, 1971; ANAHEIM, CA
    Format: text
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  • 4
    Publication Date: 2019-07-13
    Description: The impact properties of copper, copper-10 nickel, and a superalloy matrix reinforced with tungsten fibers were studied. In most cases the following increased composite impact strength: increased fiber or matrix toughness, decreased fiber-matrix reaction, increased test temperature, hot working and heat treatment. Notch sensitivity was reduced by increasing fiber or matrix toughness. The effect of fiber content depended on the relative toughness of the fibers and matrix. Above 530 K a 60 volume per cent superalloy matrix composite had a greater impact strength than a turbine blade superalloy, whereas below 530 K a hot worked 56 volume per cent composite had a greater impact strength than the superalloy.
    Keywords: MATERIALS, METALLIC
    Type: Composite materials: Testing and design; Second Conference; Apr 20, 1971 - Apr 22, 1971; Anaheim, CA
    Format: text
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