Research on the Dynamic Buckling Characteristics of Carbon Fiber Composite Honeycomb Panel under Out-of-Plane Impact Load

Ming Jun Fan

doi:10.4028/www.scientific.net/AMR.1004-1005.492

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HomeAdvanced Materials ResearchAdvanced Materials Research Vols. 1004-1005Research on the Dynamic Buckling Characteristics...

Research on the Dynamic Buckling Characteristics of Carbon Fiber Composite Honeycomb Panel under Out-of-Plane Impact Load

Abstract:

This paper aims at studying the dynamic buckling characteristic of the fiber composite honeycomb under out-of-plane impact load. It was found that: with the increasing of the wall thickness, both the critical buckling load and the critical failure load of the composite honeycomb will decrease gradually. By increasing the wall aspect, the critical buckling load will decrease, while the critical failure load will increase. However, when the aspect reaches to 3.5,both the above two kinds of load are no longer sensitive to the variation of it.

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Periodical:

Advanced Materials Research (Volumes 1004-1005)

Pages:

492-496

DOI:

https://doi.org/10.4028/www.scientific.net/AMR.1004-1005.492

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Online since:

August 2014

Authors:

Ming Jun Fan

Keywords:

Composite, Dynamic Buckling, Honeycomb, Impact

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References

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