Flutter and buckling characteristics and active control of sandwich panels with triangular lattice core in supersonic airflow

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Flutter and buckling characteristics and active control of sandwich panels with triangular lattice core in supersonic airflow

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作者：Zhi-Guang Song^a ; Feng-Ming Li^a ; ^b ; ^{fmli@bjut.edu.cn" class="auth_mail" title="E-mail the corresponding author}
关键词：Sandwich panel ; Triangular lattice core ; Flutter ; Buckling ; Yawed flow angle ; Active control
刊名：Composites Part B: Engineering
出版年：2017
出版时间：1 January 2017
年：2017
卷：108
期：Complete
页码：334-344
全文大小：3877 K

文摘

•: Flutter and buckling behaviors of sandwich panels with triangular lattice core are studied.
•: Effects of aerodynamic pressure on frequency and mode of sandwich panel are analyzed.
•: Effects of yawed flow angle on flutter characteristics of sandwich panel are researched.
•: The flutter and buckling properties of sandwich and isotropic panels are compared.

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