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International Journal of Aerospace Engineering
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International Journal of Aerospace Engineering
/
2019
/
Article
/
Tab 4
/
Research Article
Free Vibration of Composite Thin-Walled Beams with Chordwise Asymmetric Closed Cross-Sections
Table 4
Nonzero stiffness coefficients of Model A.
CUS
Different values
,
,
,
,
,
Same values
,
,
,
,
,
,
,
Only
or
,
,
,
,
,
CAS
Different values
,
,
,
Same values
,
,
,
,
,
,
,
,
,
Only
or
,
,
,
,
,
,
,
,
,