View source for SSC Aluminum: Al 1100 alloy

[[Image:Al1100.PNG]] <br> <br>


==Input Data==
[[media:S1R1N2 A1 DMG.data.txt|S1R1N2 A1 DMG.data.txt]] <br>
[[media:S1R1P0 A1 DMG.data.txt|S1R1P0 A1 DMG.data.txt]] <br>
[[media:S1R3P1 A1 DMG.data.txt|S1R3P1 A1 DMG.data.txt]] <br>
[[media:S1R3P2 A1 DMG.data.txt|S1R3P2 A1 DMG.data.txt]] <br>
[[media:T1R4P2 A1 DMG.data.txt|T1R4P2 A1 DMG.data.txt]] <br>
[[media:T2R4P2 A1 DMG.data.txt|T2R4P2 A1 DMG.data.txt]] <br>
[[media:T3R4P2 A1 DMG.data.txt|T3R4P2 A1 DMG.data.txt]] <br>

==References==
1. Holt, D.L., Babcock, S.G. Green, S.J. and Maiden, C.J., The Strain Rate Dependence of the 
Flow Stress in Some Aluminum Alloys, General Motors Research Laboratories, TR66-75, 1996. <br>

2. Horstemeyer, M.F. and Ramaswamy, S., “On Factors Affecting Localization and Void Growth 
in Ductile Metals: A Parametric Study,” Int. J. Damage Mech., Vol. 9, pp. 6-28, 2000. <br>

3. 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. <br>

4. 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.




[[Category: Aluminum]]
[[Category: Materials]]
[[Category: Metals]]