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International Journal of Aerospace Engineering
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International Journal of Aerospace Engineering
/
2016
/
Article
/
Tab 2
/
Research Article
Flutter and Thermal Buckling Analysis for Composite Laminated Panel Embedded with Shape Memory Alloy Wires in Supersonic Flow
Table 2
Comparison of critical buckling temperature for composite panel.
Ply angle
(°C)
Matsunaga [
22
]
Present
6.8
6.79
0/45/−45/90
7.6
7.59