Abstract
The paper addresses the elastic response of composite sandwich panels to local
dynamic loading. The plane and axisymmetric formulations are considered; no
overall bending is assumed. The governing equations are derived using the static
Lamé equations for the core and the plate Kirchoff-Love dynamic theory for the
faces. The closed form solutions for the non-stationary excitation are obtained
using integral transformations technique. The solutions allow to predict the stressstrain state of the structure and are in good agreement with finite element analysis.
Original language | Undefined |
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Number of pages | 10 |
Publication status | Published - 2003 |
Event | 10th International Congress on Sound and Vibration, ICSV 2003 - Stockholm, Sweden Duration: 7 Jul 2003 → 10 Jul 2003 Conference number: 10 |
Conference
Conference | 10th International Congress on Sound and Vibration, ICSV 2003 |
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Abbreviated title | ICSV |
Country/Territory | Sweden |
City | Stockholm |
Period | 7/07/03 → 10/07/03 |
Keywords
- IR-75521