Experimental analysis and modeling of the crushing of honeycomb cores
In the aeronautical field, sandwich structures are widely used for secondary structures like flaps or landing gear doors. The modeling of low velocity/low energy impact, which can lead to a decrease of the structure strength by 50%, remains a designer’s main problem. Since this type of impact has th...
| Main Authors: | , , , |
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| Format: | Article |
| Language: | English |
| Published: |
Springer
2005
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| Subjects: | |
| Online Access: | http://irep.iium.edu.my/6286/1/applied_composite_2005.pdf |