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1
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38349136027
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Repair of Mirage iii aircraft using BFRP crack patching technology
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Baker A.A., Callinan R.J., Davis M.J., Jones R., Williams J.G. Repair of Mirage iii aircraft using BFRP crack patching technology. Theor. Appl. Fracture Mech. 2:1984;1-16.
-
(1984)
Theor. Appl. Fracture Mech.
, vol.2
, pp. 1-16
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-
Baker, A.A.1
Callinan, R.J.2
Davis, M.J.3
Jones, R.4
Williams, J.G.5
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2
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0021600073
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Repair of cracked or defective metallic components with advanced fiber composites: An overview of Australian work
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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.
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(1984)
Compos. Struct.
, vol.2
, pp. 153-181
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Baker, A.A.1
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5
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0003285041
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Fatigue studies related to the certification of composite crack patching for primary metallic aircraft structures
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28-30 August, Atlanta
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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.
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(1996)
FAA-NASA Symposium on Continued Airworthiness of Aircraft Structures
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Baker, A.A.1
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7
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0003228582
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Joining and repair of aircraft composite structures
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P.K. Mallick. New York: Marcel Decker
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Baker A.A. Joining and repair of aircraft composite structures. Mallick P.K. Part 14. Composite Engineering Handbook. 1997;Marcel Decker, New York.
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(1997)
Part 14. Composite Engineering Handbook
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Baker, A.A.1
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8
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0036624128
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Computation of the stress intensity factors for repaired cracks with a bonded composite patch in mode I and mixed mode
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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
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Bachir Bouiadjra, B.1
Belhouari, M.2
Serier, B.3
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9
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0033303914
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Composites repairs to rib stiffened panels
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Ting T., Jones R., Chiu W.K., Marshall I.H., Greer J.M. Composites repairs to rib stiffened panels. Compos. Struct. 47:1999;737-743.
-
(1999)
Compos. Struct.
, vol.47
, pp. 737-743
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-
Ting, T.1
Jones, R.2
Chiu, W.K.3
Marshall, I.H.4
Greer, J.M.5
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10
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0032686270
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Composite repairs to crack in metallic components
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R. Jones, W.K. Chiu, Composite repairs to crack in metallic components, Compos. Struct. 44 (1999) 17-29.
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(1999)
Compos. Struct.
, vol.44
, pp. 17-29
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Jones, R.1
Chiu, W.K.2
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11
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0032673561
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Modelling of patch repairs to a thin cracked sheet
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V.R.S. Turaga, S. Ripudaman, Modelling of patch repairs to a thin cracked sheet, Eng. Fract. Mech. 62 (1999) 267-289.
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(1999)
Eng. Fract. Mech.
, vol.62
, pp. 267-289
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Turaga, V.R.S.1
Ripudaman, S.2
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14
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0019392130
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An application of the inclusion analogy for bonded reinforcements
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Rose L.R.F. An application of the inclusion analogy for bonded reinforcements. Int. J. Solid Struct. 17:1981;827-838.
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(1981)
Int. J. Solid Struct.
, vol.17
, pp. 827-838
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Rose, L.R.F.1
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15
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0033304354
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Bonded composite repair for fatigue-cracked primary aircraft structure
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Baker A.A. Bonded composite repair for fatigue-cracked primary aircraft structure. Compos. Struct. 74:1999;431-443.
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(1999)
Compos. Struct.
, vol.74
, pp. 431-443
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Baker, A.A.1
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