Damage evolution in fuselage stiffened composite panels under asymmetrical bending loading conditions
2017 ◽
Vol 100
◽
pp. 308-321
◽
Keyword(s):
2014 ◽
Vol 7
(3)
◽
pp. 247-256
2016 ◽
Vol 87
◽
pp. 111-119
◽
Keyword(s):