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Volumn 29, Issue 4, 2004, Pages 407-413

Disbond effect on the stress intensity factor for repairing cracks with bonded composite patch

Author keywords

[No Author keywords available]

Indexed keywords

ADHESIVES; COMPOSITE MATERIALS; CRACKS; FINITE ELEMENT METHOD; MATHEMATICAL MODELS; POLYNOMIALS; RESIDUAL STRESSES; STRESS ANALYSIS;

EID: 1642352523     PISSN: 09270256     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.commatsci.2003.11.001     Document Type: Article
Times cited : (19)

References (16)
  • 2
    • 0021600073 scopus 로고
    • Repair of cracked or defective metallic components with advanced fiber composites: An overview of Australian work
    • Baker A.A. Repair of cracked or defective metallic components with advanced fiber composites: an overview of Australian work. Compos. Struct. 2:1984;153-181.
    • (1984) Compos. Struct. , vol.2 , pp. 153-181
    • Baker, A.A.1
  • 5
    • 0003285041 scopus 로고    scopus 로고
    • Fatigue studies related to the certification of composite crack patching for primary metallic aircraft structures
    • 28-30 August, Atlanta
    • A.A. Baker, Fatigue studies related to the certification of composite crack patching for primary metallic aircraft structures, in: FAA-NASA Symposium on Continued Airworthiness of Aircraft Structures, 28-30 August 1996, Atlanta.
    • (1996) FAA-NASA Symposium on Continued Airworthiness of Aircraft Structures
    • Baker, A.A.1
  • 7
    • 0003228582 scopus 로고    scopus 로고
    • Joining and repair of aircraft composite structures
    • P.K. Mallick. New York: Marcel Decker
    • Baker A.A. Joining and repair of aircraft composite structures. Mallick P.K. Part 14. Composite Engineering Handbook. 1997;Marcel Decker, New York.
    • (1997) Part 14. Composite Engineering Handbook
    • Baker, A.A.1
  • 8
    • 0036624128 scopus 로고    scopus 로고
    • Computation of the stress intensity factors for repaired cracks with a bonded composite patch in mode I and mixed mode
    • Bachir Bouiadjra B., Belhouari M., Serier B. Computation of the stress intensity factors for repaired cracks with a bonded composite patch in mode I and mixed mode. Compos. Struct. 56:2002;401-406.
    • (2002) Compos. Struct. , vol.56 , pp. 401-406
    • Bachir Bouiadjra, B.1    Belhouari, M.2    Serier, B.3
  • 10
    • 0032686270 scopus 로고    scopus 로고
    • Composite repairs to crack in metallic components
    • R. Jones, W.K. Chiu, Composite repairs to crack in metallic components, Compos. Struct. 44 (1999) 17-29.
    • (1999) Compos. Struct. , vol.44 , pp. 17-29
    • Jones, R.1    Chiu, W.K.2
  • 11
    • 0032673561 scopus 로고    scopus 로고
    • Modelling of patch repairs to a thin cracked sheet
    • V.R.S. Turaga, S. Ripudaman, Modelling of patch repairs to a thin cracked sheet, Eng. Fract. Mech. 62 (1999) 267-289.
    • (1999) Eng. Fract. Mech. , vol.62 , pp. 267-289
    • Turaga, V.R.S.1    Ripudaman, S.2
  • 14
    • 0019392130 scopus 로고
    • An application of the inclusion analogy for bonded reinforcements
    • Rose L.R.F. An application of the inclusion analogy for bonded reinforcements. Int. J. Solid Struct. 17:1981;827-838.
    • (1981) Int. J. Solid Struct. , vol.17 , pp. 827-838
    • Rose, L.R.F.1
  • 15
    • 0033304354 scopus 로고    scopus 로고
    • Bonded composite repair for fatigue-cracked primary aircraft structure
    • Baker A.A. Bonded composite repair for fatigue-cracked primary aircraft structure. Compos. Struct. 74:1999;431-443.
    • (1999) Compos. Struct. , vol.74 , pp. 431-443
    • Baker, A.A.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.