Free vibration analysis of composite aircraft wings modeled as thin-walled beams with NACA airfoil sections
Keyword(s):
Keyword(s):
Keyword(s):
2008 ◽
Vol 46
(10)
◽
pp. 1107-1112
◽
2015 ◽
Vol 2015
◽
pp. 1-12
◽
1995 ◽
Vol 181
(3)
◽
pp. 503-513
◽
Keyword(s):
2008 ◽
Vol 86
(6)
◽
pp. 573-579
◽
Keyword(s):
2013 ◽
Vol 332
(23)
◽
pp. 6104-6127
◽
Keyword(s):