Cite
HARVARD Citation
Solob, A. et al. (2020). XFEM based analysis of fatigue crack growth in damaged wing-fuselage attachment lug. Engineering failure analysis. p. . [Online].
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Solob, A. et al. (2020). XFEM based analysis of fatigue crack growth in damaged wing-fuselage attachment lug. Engineering failure analysis. p. . [Online].