Integrated Computational Materials Engineering (ICME)

SSC Titanium: Ti0Al6V4 Titanium Alloy

Figure 1

Input Data

C1R1P0 B1 DMG.data.txt
C1R1P3 B1 DMG.data.txt
C1R4N3 B1 DMG.data.txt
C1R8N2 B1 DMG.data.txt
T1R4N4 B1 DMG.data.txt
T1R4P0 B1 DMG.data.txt

References

  1. Department of Defense. Military Standardization Handbook: Metallic Materials and Elements for Aerospace Vehicle Structures MIL-HDBK-5E, Volume 2. June 1987.
  2. Johnson, G.R. and Holmquist, T.J., Test data and computational strength and fracture model constants for 23 materials subjected to large strains, high strain rates, and high temperatures, LA- 11463-MS, Los Alamos National Laboratory, 1989.
  3. Nicholas, T., Material behavior at high strain rates, Report AFWAL-TR-80-4053, USAF Wright Aeronautical Laboratories, Wright-Patterson Air Force Base, OH, USA, 1980.
  4. Maiden and Green