1. XFEM based analysis of fatigue crack growth in damaged wing-fuselage attachment lug. (May 2020) Authors: Solob, A.; Grbović, Aleksandar; Božić, Ž.; Sedmak, S.A. Journal: Engineering failure analysis Issue: Volume 112(2020) Page Start: Record Type: Journal Article View Content: Available online (eLD content is only available in our Reading Rooms) ↗