Identifying flow defects in amorphous alloys using machine learning outlier detection methods
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Materials Science↗
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Results for “ALLOY”
Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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Strong and ductile nanoscale Ti-1Fe dual-phase alloy via deformation twinning
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Materials Science↗
Corrosion Characteristics of Typical Ni–Cr Alloys and Ni–Cr–Mo Alloys in Supercritical Water: A Review
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Guo, Shuwei↗
Stabilization of a nanoporous NiCu dilute alloy catalyst for non-oxidative ethanol dehydrogenation
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99 GENERAL AND MISCELLANEOUS↗
Advanced Fuel Cycle Cost Basis Report: Module D1-6A Contact-Handled All-U Metal or U-Metal Alloy Uranium Fuel Fabrication Module D1-6B Contact-Handled U,Pu Metal Alloy Fuel Fabrication
Advanced Fuel Cycle Cost Basis Report cost module on contact handled fuel.
11 NUCLEAR FUEL CYCLE AND FUEL MATERIALS↗
ALLOY EXPRESS: A General and Scalable parallel Hybrid Monte Carlo and Molecular Dynamics Algorithm for Alloy Simulations
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Zichi, Laura Rose [Sandia National Laboratories (S↗
High temperature, low-cycle fatigue of copper-base alloys in argon. Part 1: Preliminary results for 12 alloys at 1000 F (538 C)
Short-term tensile evaluations at room temperature and 538 C and low-cycle fatigue evaluations at 538 C are presented for the following materials: Zirconium copper-annealed, Zirconium copper-1/4 hard, Zirconium copper-1/2 hard, Tellurium copper-1/2 hard, Chromium copper-SA and aged, OFHC copper-hard, OFHC copper-1/4 hard, OFHC copper-annealed, Silver-as drawn, Zr-Cr-Mg copper-SA, CW and aged, Electroformed copper-30-35 ksi, and Co-Be-Zr- copper-SA, aged. A total of 50 tensile tests and 76 low-cycle fatigue tests were performed using a strain rate of 0.2 percent per second.
Conway, J. B.↗
The effects of alloy composition on the salt-water stress-corrosion susceptibility of titanium-aluminum-base alloys
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Wood, R. A.↗
The cyclic oxidation resistance of cobalt chromium-aluminum alloys at 1100 and 1200 C and a comparison with the nickel-chromium-aluminum alloy system
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Barrett, C. A.↗
Rupture properties of low carbon N-155 type alloys made with a columbium-tantalum ferro-alloy
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Freeman, J W↗
Wear and Sliding Friction Properties of Nickel Alloys Suited for Cages of High-temperature Rolling-contact Bearings I : Alloys Retaining Mechanical Properties to 600 F
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CONTACT SURFACES, SLIDING↗
Wear and Sliding Friction Properties of Nickel Alloys Suited for Cages of High-temperature Rolling-contact Bearings II : Alloys Retaining Mechanical Properties Above 600 F
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FRICTION AND LUBRICATION - SURFACE CONDITIONS↗
NASA Developed High Temperature AM Alloys - Presenting NX810: An Additively Manufactured Oxide Dispersion Strengthened Alloy
Problem: Conventional materials and processing techniques limit the design and operating temperature of aerospace components. Proposed Solution: Develop a high temperature capable material that can be additively manufactured and can operate in temperatures above 2000°F (1093°C)
Timothy M. Smith↗