Figure 8From: Fatigue Property of Additively Manufactured Ti-6Al-4V under Nonproportional Multiaxial LoadingHysteresis loops obtained at 0.5 Nf for Δεeq = 1.3% of a PP HT and b PP NHT and Δεeq = 0.5% of c CI HT and d CI NHT, and maximum stress for Δεeq = 1.3% of e PP path, maximum stress for Δεeq = 0.5% of f CI pathBack to article page