adhesive prepreg
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2016 ◽  
Vol 35 (21) ◽  
pp. 1566-1575 ◽  
Author(s):  
Chao Chen ◽  
Yanxia Li ◽  
Yizhuo Gu ◽  
Min Li ◽  
Zuoguang Zhang

2014 ◽  
Vol 7 (2) ◽  
pp. 81-83 ◽  
Author(s):  
L. I. Anikhovskaya ◽  
D. V. Batizat ◽  
E. I. Baturina ◽  
E. V. Leshchun ◽  
A. M. Sakharov

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.


2008 ◽  
Vol 15 (1) ◽  
pp. 47-59 ◽  
Author(s):  
Chongxin Yuan ◽  
Min Li ◽  
Zuoguang Zhang ◽  
Yizhuo Gu

2007 ◽  
Vol 49 (2) ◽  
pp. 166-170
Author(s):  
O. V. Startsev ◽  
A. S. Krotov ◽  
N. V. Ponomareva ◽  
L. I. Anikhovskaya ◽  
D. V. Batizat ◽  
...  

TANSO ◽  
1992 ◽  
Vol 1992 (155) ◽  
pp. 398-402 ◽  
Author(s):  
Isao Mochida ◽  
Ryuji Fujiura ◽  
Yozo Korai

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