- 충격손상을 받은 항공기용 복합재료의 잔류강도 평가
- ㆍ 저자명
- 최정훈,강민성,신인환,구재민,석창성,Choi. Jung-Hun,Kang. Min-Sung,Shin. In-Hwan,Koo. Jae-Mean,Seok. Chang-Sung
- ㆍ 간행물명
- 한국정밀공학회지
- ㆍ 권/호정보
- 2010년|27권 2호|pp.94-101 (8 pages)
- ㆍ 발행정보
- 한국정밀공학회
- ㆍ 파일정보
- 정기간행물| PDF텍스트
- ㆍ 주제분야
- 기타
Composite materials have a higher specific strength and modulus than traditional metallic materials. Additionally, these materials offer new design flexibilities, corrosion and wear resistance, low thermal conductivity and increased fatigue life. These, however, are susceptible to impact damage due to their lack of through-thickness reinforcement and it causes large drops in the load-carrying capacity of a structure. Therefore, the impact damage behavior and subsequently load-carrying capacity of impacted composite materials deserve careful investigation. In this study, the residual strength and impact characteristics of plain-woven CFRP composites with impact damage are investigated under axial tensile test. Impact test was performed using drop weight impact tester. And residual strength behavior by impact was evaluated using the caprino model. Also we evaluated behavior of residual strength by change of mass and size of impactor. Examined change of residual strength by impact energy change through this research and consider impactor diameter in caprino model.