Numerical Investigation of Dynamic Response and Failure Mechanisms for Composite Lattice Sandwich Structure under Different Slamming Loads

Author(s):  
Wentao He ◽  
Jun Wu ◽  
Lu Yao ◽  
Changzi Wang ◽  
Hao Zhang ◽  
...  
2011 ◽  
Vol 46 (12) ◽  
pp. 1417-1430 ◽  
Author(s):  
Yu-Ti Jhan ◽  
Ya-Jung Lee ◽  
Cheng-Hsien Chung

2010 ◽  
pp. 223-235

Abstract The honeycomb sandwich structure composite is a very efficient and complex structure widely used in the aircraft industry. Honeycomb-cored sandwich panels increase part stiffness at a lower weight than monolithic composite materials. This chapter describes the analysis of the intermingling of the film adhesive/prepreg resin system. It discusses the causes and effects of honeycomb core movement, which results in core crush. The chapter also explains the formation of a void in honeycomb composites and the failure mechanisms in honeycomb sandwich structure composites.


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