Browse > Article
http://dx.doi.org/10.7234/kscm.2007.20.5.001

Comparative Study on Low-velocity Impact Behavior of Graphite/Epoxy Composite laminate and Steel Plate  

Kong, Chang-Duk (조선대학교 항공우주공학과)
Kim, Yeong-Gwang (조선대학교 항공우주공학과)
Lee, Seung-Hyeon (조선대학교 항공우주공학과)
Publication Information
Composites Research / v.20, no.5, 2007 , pp. 1-6 More about this Journal
Abstract
This study was performed to make a comparison on low-velocity impact behavior between graphite/epoxy composite laminate and steel plate. In order to validate the proposed scheme fur the impact behavior of the plate, the Karas's impact model was used. The impact models for this comparative study are the graphite/epoxy composite plate having $[0/90/45/-45/-45/45/90/0]_{8S}$ laminate sequence and the steel plate with a steel ball impactor. The low-velocity impact behaviors for two types of plates were comparatively investigated and performed by considering different impactor velocities and weights respectively. In this investigation, it was found that the composite laminate has impact energy absorption effect due to more flexible behavior than the steel plate, and also it has better characteristics on impact damage and weight.
Keywords
Low-velocity Impact; Impact Behavior; Composite Plate; Steel Plate;
Citations & Related Records
Times Cited By KSCI : 1  (Citation Analysis)
연도 인용수 순위
1 W. J. Stronge, 'Impact Mechanics,' Cambridge University Press, 2000
2 최익현, 홍창선, '복합적층판의 저속충격 손상영역 평가,' 한국항공우주학회지, 제22권, 제4호, 1994, pp. 78-88
3 최익현, '복합적층판에 대한 저속충격해석과 접촉법칙,' 한국복합재료학회지, 제16권, 제1호, 2003, pp. 50-57
4 박정, 박훈철, 윤광준, 구남서, 이재화, '가정변형률 솔리드 요소를 이용한 복합재 샌드위치 평판의 저속충격 해석,' 한국항공우주학회지, 제30권, 제7호, 2002, pp. 44-50
5 K. Karas, 'Platten Unter Seitlichem Stob,' Ingeieur Archiv, Vol. 10, 1939, pp. 237-250   DOI
6 고종인, 홍창선, 이인, '저속충격에 의한 복합 적층판의 손상해석', 한국항공우주학회지, 제19권, 제1호, 1991, pp. 35-40