최소 단어 이상 선택하여야 합니다.
최대 10 단어까지만 선택 가능합니다.
다음과 같은 기능을 한번의 로그인으로 사용 할 수 있습니다.
NTIS 바로가기Theoretical and applied fracture mechanics, v.2 no.1, 1984년, pp.1 - 15
Baker, A.A. , Callinan, R.J. , Davis, M.J. , Jones, R. , Williams, J.G.
The BFRP crack-patching technique has been applied to the field repair of fatigue cracks in the aluminium alloy wing skins of Mirage III fighter aircraft. Finite-element procedures were used in patch design. The repair was qualified using fatigue-crack propagation studies on panels simulating the cr...
Composites Baker Vol. 9 11 1978 10.1016/0010-4361(78)90512-8
Baker 1978 Proceedings of 33rd Annual Technical Conference of the Plastics Industry Fibre composite reinforcement of cracked aircraft structures
J. Struct. Mech. Jones Vol. 7 107 1979 10.1080/03601217908905315
A.I.A.A. Mitchell Vol. 13 744 1975
S.A.M.P.E. Journal Baker Vol. 15 10 1979
Baker 1979 Proceedings of the 10th International Committee on Aeronautical Fatigue Symposium Repair of fatigue cracked aircraft structures with advanced fibre composites: Residual stress and thermal fatigue studies
J. Fibre Science and Technology Jones Vol. 14 99 1981 10.1016/0015-0568(81)90035-X
J. Struct. Mech. Jones Vol. 8 143 1980 10.1080/03601218008907356
Locke 1975 7th S.A.M.P.E. Tech. Conf. Non-tank phosphoric anodize method of surface preparation for repair bonding
R.A.E. Reports and Memoranda No. 3798 Hart-Smith 1975 Effects of heat on fatigue in aircraft structure
Int. J. Fracture Jones Vol. 13 51 1977 10.1007/BF00040875
Jones 1977 Proc. 4th Int. Conf. in Australia on Finite Element Methods Hybrid elements and elastic plastic fracture mechanics
*원문 PDF 파일 및 링크정보가 존재하지 않을 경우 KISTI DDS 시스템에서 제공하는 원문복사서비스를 사용할 수 있습니다.
※ AI-Helper는 부적절한 답변을 할 수 있습니다.