DocumentCode :
2942488
Title :
Comparison of Artificial Neural Networks with Response Surface Models in Characterizing the Impact Damage Resistance of Sandwich Airframe Structures
Author :
Li, Jian ; Chen, Xiuhua ; Wang, Hai
Author_Institution :
Sch. of Aeronaut. & Astronaut., Shanghai Jiaotong Univ., Shanghai, China
Volume :
2
fYear :
2009
fDate :
12-14 Dec. 2009
Firstpage :
210
Lastpage :
215
Abstract :
In the development of a damage tolerance plan for composite airframe structures, the way to characterize the impact damage of sandwich composites under different levels of impact events and material property is crucial. The aim of the present research is to investigate the influence of material configuration and impact parameters on damage resistance responses of composite sandwich structures comprised of carbon-epoxy woven fabric facesheets and Nomex honeycomb cores. Two methods, artificial neural network and classic response surface methodology were used to predict the relationship between the impact damage response and its dependent parameters. The results obtained through artificial neural networks were compared with those through response surface methodology.
Keywords :
aerospace components; carbon; honeycomb structures; impact (mechanical); neural nets; response surface methodology; sandwich structures; structural engineering computing; woven composites; C; Nomex honeycomb cores; artificial neural networks; carbon-epoxy woven fabric facesheets; damage tolerance plan; impact damage resistance; material configuration; response surface models; sandwich airframe structures; Aerospace industry; Analytical models; Artificial neural networks; Composite materials; Manufacturing; Response surface methodology; Sandwich structures; Sheet materials; Stress; Surface resistance;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Computational Intelligence and Design, 2009. ISCID '09. Second International Symposium on
Conference_Location :
Changsha
Print_ISBN :
978-0-7695-3865-5
Type :
conf
DOI :
10.1109/ISCID.2009.200
Filename :
5371076
Link To Document :
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