A methodology for fatigue crack growth and residual strength prediction with applications to aircraft fuselages
Keyword(s):
1984 ◽
Vol 7
(4)
◽
pp. 329-344
◽
Keyword(s):
2008 ◽
Vol 33-37
◽
pp. 261-266
Keyword(s):
2001 ◽
Vol 11
(PR5)
◽
pp. Pr5-69-Pr5-75