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Finite Element Analysis Simulation of a Fireproof Test for an Aircraft Propulsion Engine Mount Structure Made of Titanium

Journal Article
2015-01-2621
ISSN: 1946-3855, e-ISSN: 1946-3901
DOI: https://doi.org/10.4271/2015-01-2621
Published September 15, 2015 by SAE International in United States
Finite Element Analysis Simulation of a Fireproof Test for an Aircraft Propulsion Engine Mount Structure Made of Titanium
Sector:
Citation: Leicht, D., "Finite Element Analysis Simulation of a Fireproof Test for an Aircraft Propulsion Engine Mount Structure Made of Titanium," SAE Int. J. Aerosp. 8(1):117-122, 2015, https://doi.org/10.4271/2015-01-2621.
Language: English

References

  1. United States Department of Transportation - Federal Aviation Administration Federal Aviation Regulations (FAR) 14 CFR 23 and 25, Office of the Secretary, Distribution Service Branch, M-484.1 Washington, DC 20590
  2. Federal Aviation Administration Advisory Circular AC No: 20-135 February 6
  3. Code of Federal Regulations (CFR) Title 14-Aeronautics and Space, Part 1-Definitions and Abbreviations 2010
  4. SAE AMS4928Q Titanium Alloy Bars, Wire, Forgings, Rings, and Drawn Shapes 6AL-4V Annealed SAE International Aerospace Material Specification April 2001
  5. SAE AMS-H-81200B Heat Treatment of Titanium and Titanium Alloys SAE International Aerospace Material Specification July 13 2003
  6. ANSYS® Mechanical Release 11 Finite Element Software ANSYS, Inc 2009
  7. MIL-HDBK-5H Metallic Materials and Elements for Aerospace Vehicle Structures December 1 1998
  8. The Engineering Toolbox Air Flow and Velocities due to Natural Draft http://www.engineeringtoolbox.com/natural-draught-ventilation-d_122.html
  9. Incropera , F.P. , DeWitt , D.P. Fundamentals of Heat and Mass Transfer 4th 1996
  10. MIL-HDBK-697A Military Handbook: Titanium and Titanium Alloys June 1 1974

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