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Volumn 60, Issue 1, 2003, Pages 1-7

A study on the fatigue crack growth behaviour of thick aluminum panels repaired with a composite patch

Author keywords

[No Author keywords available]

Indexed keywords

CRACK PROPAGATION; FIBER REINFORCED MATERIALS; FINITE ELEMENT METHOD; STRESSES; STRUCTURAL PANELS;

EID: 0037400083     PISSN: 02638223     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0263-8223(02)00338-0     Document Type: Article
Times cited : (38)

References (17)
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    • Rastogi, N.1    Soni, S.R.2    Denny, J.J.3
  • 2
    • 84987486552 scopus 로고
    • Repair efficiency in fatigue-cracked aluminum components reinforced with boron/epoxy patches
    • Baker AA. Repair e.ciency in fatigue-cracked aluminum components reinforced with boron/epoxy patches. Fatigue Fract Eng Mater Struct 1993;16:753-65.
    • (1993) Fatigue Fract Eng Mater Struct , vol.16 , pp. 753-765
    • Baker, A.A.1
  • 4
    • 0031182320 scopus 로고    scopus 로고
    • Characterization of disbond effects on fatigue crack growth behavior in aluminum plate with bonded composite patch
    • Denney JJ, Mall S. Characterization of disbond effects on fatigue crack growth behavior in aluminum plate with bonded composite patch. Eng Fract Mech 1997;57:507-25.
    • (1997) Eng Fract Mech , vol.57 , pp. 507-525
    • Denney, J.J.1    Mall, S.2
  • 5
    • 0013426165 scopus 로고
    • Analysis of composite patching of fuselage structures: High patch elastic modulus isn't the whole story
    • Anaheim, CA, April 11-14
    • Fredell R, Barneveld WV, Volt A. Analysis of composite patching of fuselage structures: high patch elastic modulus isn't the whole story. In: Proceedings of the 39th International SAMPE Symposium, Anaheim, CA, April 11-14, 1994. p. 610-23.
    • (1994) Proceedings of the 39th International SAMPE Symposium , pp. 610-623
    • Fredell, R.1    Barneveld, W.V.2    Volt, A.3
  • 6
    • 0004017822 scopus 로고    scopus 로고
    • Airtask no. wf41-400, PE 62241, report no. NADC-82139-60, United States Navy Air Development Center, Warminster, PA
    • Kan HP, Ratwani MM. Composite patch repair of thick aluminum structures final report. Airtask no. WF41-400, PE 62241, report no. NADC-82139-60, United States Navy Air Development Center, Warminster, PA 18974, 1983.
    • Composite Patch Repair of Thick Aluminum Structures Final Report , pp. 1983
    • Kan, H.P.1    Ratwani, M.M.2
  • 9
    • 0031247090 scopus 로고    scopus 로고
    • Fatigue crack growth analysis of adhesively repaired panel using perfectly and imperfectly composite patches
    • Noboulsi S, Mall S. Fatigue crack growth analysis of adhesively repaired panel using perfectly and imperfectly composite patches. Theor Appl Fract Mech 1997;28:13-28.
    • (1997) Theor Appl Fract Mech , vol.28 , pp. 13-28
    • Noboulsi, S.1    Mall, S.2
  • 10
    • 0032660852 scopus 로고    scopus 로고
    • Investigation of a cracked thick aluminum panel repaired with a bonded composite patch
    • Schubbe JJ, Mall S. Investigation of a cracked thick aluminum panel repaired with a bonded composite patch. Eng Fract Mech 1999;63:305-23.
    • (1999) Eng Fract Mech , vol.63 , pp. 305-323
    • Schubbe, J.J.1    Mall, S.2
  • 11
    • 0033752591 scopus 로고    scopus 로고
    • Investigation of the size effect of composite patching repaired on edge-cracked plates
    • Wang W-C, Hsu J-S. Investigation of the size effect of composite patching repaired on edge-cracked plates. Compos Struct 2000;49:415-23.
    • (2000) Compos Struct , vol.49 , pp. 415-423
    • Wang, W.-C.1    Hsu, J.-S.2
  • 12
    • 0033722375 scopus 로고    scopus 로고
    • Fracture mechanics analysis of cracked plate repaired by composite patch
    • Chung KH, Yang WH, Cho MR. Fracture mechanics analysis of cracked plate repaired by composite patch. Key Eng Mater 2000;183-187:43-8.
    • (2000) Key Eng Mater , vol.183-187 , pp. 43-48
    • Chung, K.H.1    Yang, W.H.2    Cho, M.R.3
  • 13
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  • 14
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    • Fracture mechanics analysis of cracked plate repaired by patch (2)-The analysis of debonding effect
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    • Chung, K.H.1    Yang, W.H.2    Cho, M.R.3
  • 15
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  • 17
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.