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Factors influencing the formation of soft particles in biodiesel

  • Technical Paper
  • 2020-24-0006
To be published on 2020-09-27 by SAE International in United States
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Problems of using residual fuels on the wear of selected elements of self-ignition internal combustion engines

  • Technical Paper
  • 2020-01-2103
To be published on 2020-09-15 by SAE International in United States
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Effect of Lubricant Oil Formulation on Characteristics of Particle Emission from Engine Fed with a Hydrogen-Rich Fuel

  • Technical Paper
  • 2020-01-2200
To be published on 2020-09-15 by SAE International in United States
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Aluminum Alloy, Extrusions 6.3Cu - 0.30Mn - 0.18Zr - 0.10V - 0.06Ti (2219-T8511) Solution Treated, Stress Relief Stretched, Straightened, and Precipitation Heat Treated

  • Aerospace Material Specification
  • AMS4162F
  • Current
Published 2020-07-01 by SAE International in United States
This content contains downloadable datasets
Annotation ability available
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Titanium Alloy Wire 44.5 Cb

  • Aerospace Material Specification
  • AMS4982G
  • Current
Published 2020-07-01 by SAE International in United States
This content contains downloadable datasets
Annotation ability available
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Titanium Alloy, Bars, Wire, Forgings, and Rings 6.0Al - 4.0V Annealed, Heat Treatable, Modified Strength

  • Aerospace Material Specification
  • AMS4963E
  • Current
Published 2020-06-29 by SAE International in United States
This content contains downloadable datasets
Annotation ability available
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Steel, Bars and Forgings 2.0Cr - 10Ni - 8.0Co - 1.0Mo (0.10 - 0.14C) (HY-180) Double Vacuum Melted Solution Heat Treated, Marage Hardenable

  • Aerospace Material Specification
  • AMS6543G
  • Current
Published 2020-06-29 by SAE International in United States
This content contains downloadable datasets
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Titanium Alloy Bars, Wire, and Forgings 7Al - 4Mo Solution and Precipitation Heat Treated

  • Aerospace Material Specification
  • AMS4970L
  • Current
Published 2020-06-29 by SAE International in United States
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Aluminum Alloy, Plate 1.6Cu - 2.2Mg - 0.22Cr - 5.7Zn (7475-T7651) Solution Heat Treated, Stress Relieved by Stretching, and Precipitation Heat Treated

  • Aerospace Material Specification
  • AMS4089F
  • Current
Published 2020-06-18 by SAE International in United States
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Titanium Alloy Forgings 8Al - 1Mo - 1V Solution Heat Treated and Stabilized

  • Aerospace Material Specification
  • AMS4973J
  • Current
Published 2020-06-16 by SAE International in United States
This content contains downloadable datasets
Annotation ability available