Research Article

Free Vibration of Composite Thin-Walled Beams with Chordwise Asymmetric Closed Cross-Sections

Table 3

Stiffness coefficients of Model A and Model C.
(a)

CUS: and

1234567
1
2
3
4
5
6Sym.
7

(b)

CAS: and

1234567
1
2
3
4
5
6Sym.
7

(c)

CUS: or

1234567
1
2
3
4
5
6Sym.
7

(d)

CAS: or

1234567
1
2
3
4
5
6Sym.
7