[European Structural Integrity Society] Fatigue Design and Reliability Volume 23 || Fatigue strength of L610-P wing-fuselage attachment lug made of glare 2 fibre-metal laminate
Vašek, A.Year:
1999
Language:
english
DOI:
10.1016/S1566-1369(99)80031-4
File:
PDF, 820 KB
english, 1999