국문목차
표제지=0,1,3
목차=i,4,2
표 목차=iii,6,1
그림 목차=iv,7,1
Abstract=v,8,2
I. 서론=1,10,1
1. 연구 배경=1,10,2
2. 연구 목적 및 범위=3,12,1
II. 실험 방법=4,13,1
1. 시편 제작=4,13,1
1.1 복합재 모재=5,14,5
1.2 알루미늄 모재=10,19,2
1.3 접착제 접합 시편=12,21,3
1.4 볼트 체결 시편=15,24,2
1.5 하이브리드 체결 시편=17,26,2
2. 실험 장치 및 조건=19,28,1
III. 실험 결과 및 고찰=20,29,1
1. 접착제 접합 시편=20,29,8
2. 볼트 체결 시편=28,37,5
3. 하이브리드 체결 시편=33,42,5
4. 파손 변위 및 강도 비교=38,47,3
IV. 결론=41,50,1
참고 문헌=42,51,3
Table1. Number of specimens=4,13,1
Table2. Physical properties of carbon/epoxy composite=8,17,1
Table3. Property of aluminum 7075-T62=11,20,1
Table4. Property of adhesive=14,23,1
Table5. Test results - adhesive bonded specimens=20,29,1
Table6. Comparison of shear strength between present and previous data=26,35,1
Table7. Test results-bolted joint specimens=28,37,1
Table8. Test results-hybrid joint specimens=33,42,1
Fig.1. Procedure of bagging=5,14,1
Fig.2. Autoclave=6,15,1
Fig.3. Basic cure cycle=7,16,1
Fig.4. Composite specimens=9,18,1
Fig.5. Aluminum specimens=10,19,1
Fig.6. Adhesive and sandpaper=13,22,1
Fig.7. Configuration of adhesive bonded specimen=14,23,1
Fig.8. Sealant=16,25,1
Fig.9. Configuration of bolted joint specimen=16,25,1
Fig.10. Configuration of 3 types of specimen-front view=17,26,1
Fig.11. Configuration of 3 types of specimen-side view=18,27,1
Fig.12. Experimental set-up=19,28,1
Fig.13. Load-displacement curve of adhesive bonded joints=21,30,3
Fig.14. Failure mode of adhesive bonded specimens=27,36,1
Fig.15. Various failure modes of adhesive bonded joint=27,36,1
Fig.16. Load-displacement curve of bolted joint specimen=29,38,2
Fig.17. Failure mode of bolted joint specimens=32,41,1
Fig.18. Failure modes of bolted joint=32,41,1
Fig.19. Load-displacement curve of hybrid joint specimen=34,43,3
Fig.20. Failure mode of hybrid joint specimens=37,46,1
Fig.21. Comparison of failure displacement=38,47,1
Fig.22. Comparison of failure load=39,48,1