Supersonic flutter of sandwich panels: effects of face sheet bending stiffness, rotary inertia, and orthotropic core shear stiffnesses
A theoretical analysis is presented for the supersonic flutter of flat rectangular, biaxially stressed sandwich panels. On the basis of two-dimensional static aerodynamic theory an exact solution is obtained for panels having simply supported edges parallel to the airflow. The leading and trailing e...
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| Format: | Others |
| Language: | en |
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Virginia Polytechnic Institute and State University
2019
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| Online Access: | http://hdl.handle.net/10919/91029 |