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Computational Simulation of an Electrically Heated Ice Protection System for Composite Leading Edges of Aircraft

Gyeongsang National University-Prince Raj Lawrence Raj, Hojin Jeong, Rene Roy, Jin-Hwe Kweon, Rho Shin Myong
Published 2019-06-10 by SAE International in United States
The performance of an electrically heated aircraft ice protection system for a composite leading edge was evaluated. The composite leading edge of the model is equipped with a Ni alloy resistance heater. A state-of-the-art icing code, FENSAP-ICE, was used for the analysis of the electrothermal de-icing system. Computational results, including detailed information of conjugate heat transfer, were validated with experimental data. The computational model was then applied to the composite leading edge wing section at various metrological conditions selected from FAR Part 25 Appendix C.
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Electrical Characterization of Crystalline UO2, THO2 and U0.71TH0.29O2

Aerospace & Defense Technology: June 2019

  • Magazine Article
  • 19AERP06_08
Published 2019-06-01 by SAE International in United States

Evaluating the suitability of advanced alloys for use in uranium-based neutron detectors.

Tracking and identifying radiation sources in the age of nuclear proliferation and well-resourced non-state actors is a national priority. Current neutron detection methods favor large detector volumes and long data collection times. Additionally, portable neutron detection methods have persistent problems with low signal-to-noise (small pulse height) and require large applied voltages.

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Nickel-Iron Alloy, Magnetic, Sheet and Strip 50Ni - 50Fe Annealed, Forming Grade

AMS E Carbon and Low Alloy Steels Committee
  • Aerospace Material Specification
  • AMS7717E
  • Current
Published 2019-05-29 by SAE International in United States
This specification covers a magnetically soft nickel-iron alloy in the form of sheet and strip.
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Nickel-Iron Alloy, Magnetic, Sheet and Strip 50Ni - 50Fe Stamping Quality, Half-Hard Temper

AMS E Carbon and Low Alloy Steels Committee
  • Aerospace Material Specification
  • AMS7719E
  • Current
Published 2019-05-29 by SAE International in United States
This specification covers a magnetic nickel-iron alloy in the form of sheet and strip.
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Nickel-Iron Alloy, Magnetic, Bars, Rods, Tubing, and Forgings 50Ni - 50Fe

AMS E Carbon and Low Alloy Steels Committee
  • Aerospace Material Specification
  • AMS7718H
  • Current
Published 2019-05-29 by SAE International in United States
This specification covers a magnetically soft nickel-iron alloy in the form of bars, rods, forgings, mechanical tubing, and forging stock.
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Enhanced Ultrasonic Immersion Inspection for Titanium Alloy and other Metal Alloy Billets

AMS K Non Destructive Methods and Processes Committee
  • Aerospace Material Specification
  • AMS2628B
  • Current
Published 2019-05-16 by SAE International in United States

This specification covers procedures for ultrasonic immersion inspection of premium grade wrought titanium and titanium alloy round billet 5 inches (127 mm) and over in nominal diameter (see 8.5). Metal alloy billets other than titanium may be tested to this specification with the use of suitable reference standards.

 
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Alloy, Corrosion and Heat Resistant, Investment Castings, 30Fe - 21Cr - 20Ni - 20Co - 3.0Mo - 2.5W - 1.0Cb - 0.15N, As Cast

AMS F Corrosion Heat Resistant Alloys Committee
  • Aerospace Material Specification
  • AMS5376H
  • Current
Published 2019-05-14 by SAE International in United States

This specification covers a corrosion and heat-resistant iron alloy in the form of investment castings.

 

Copper-Nickel-Tin Alloy, Bars and Rods 77Cu - 15Ni - 8Sn Solution Annealed, Cold Finished and Spinodal Hardened (TX TS)

AMS D Nonferrous Alloys Committee
  • Aerospace Material Specification
  • AMS4597A
  • Current
Published 2019-04-30 by SAE International in United States
This specification covers a copper-nickel-tin alloy in the form of bars and rods.
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Cobalt Alloy, Corrosion and Heat Resistant, Hardfacing Rod and Wire 62Co - 27Cr - 2.9Ni - 5.5Mo

AMS F Corrosion Heat Resistant Alloys Committee
  • Aerospace Material Specification
  • AMS5819A
  • Current
Published 2019-04-30 by SAE International in United States
This specification covers a corrosion and heat-resistant cobalt alloy in the form of welding rods or wrought wire.
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CLAMP ASSEMBLY, SADDLE TYPE, CUSHIONED

G-3, Aerospace Couplings, Fittings, Hose, Tubing Assemblies
  • Aerospace Standard
  • AS8443
  • Current
Published 2019-04-29 by SAE International in United States
No Abstract Available.
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