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International Journal of Aerospace Engineering
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International Journal of Aerospace Engineering
/
2019
/
Article
/
Tab 6
/
Research Article
Free Vibration of Composite Thin-Walled Beams with Chordwise Asymmetric Closed Cross-Sections
Table 6
Mass matrix
of Model A and Model C.
(a)
CUS & CAS:
and
1
2
3
4
5
6
1
2
3
4
5
6
Sym.
(b)
CUS & CAS:
or
1
2
3
4
5
6
1
2
3
4
5
6
Sym.