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5
-
-
0344986854
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Bonded Repair to Cracking in Primary Structure: A Case Study
-
Melbourne, Australia, March
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Davis, M. J., Kearns, K. J. and Wilkin, M. O., 'Bonded Repair to Cracking in Primary Structure: A Case Study', in Proceedings PICAST2-AA6, Institution of Engineers, Melbourne, Australia, March 1995, pp. 323-330.
-
(1995)
Proceedings PICAST2-AA6, Institution of Engineers
, pp. 323-330
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-
Davis, M.J.1
Kearns, K.J.2
Wilkin, M.O.3
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6
-
-
0345418041
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The F-111 Logic: Familiar Materials; Proven Processes
-
McHenry, H. I. and Key, R. E., 'The F-111 Logic: Familiar Materials; Proven Processes', Metal Progress 93(3), 1968, 62-68.
-
(1968)
Metal Progress
, vol.93
, Issue.3
, pp. 62-68
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-
McHenry, H.I.1
Key, R.E.2
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7
-
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0344124309
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Design Validation for a Bonded Composite Repair to the F-111 Lower Wing Skin
-
Institution of Engineers, Melbourne, Australia, March
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Rose, L. R. F., Callinan, R. J., Baker, A. A., Sanderson, S. and Wilson, E. S., 'Design Validation for a Bonded Composite Repair to the F-111 Lower Wing Skin', in Proceedings PICAST2-AAC6, Institution of Engineers, Melbourne, Australia, March 1995, pp. 331-336.
-
(1995)
Proceedings PICAST2-AAC6
, pp. 331-336
-
-
Rose, L.R.F.1
Callinan, R.J.2
Baker, A.A.3
Sanderson, S.4
Wilson, E.S.5
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9
-
-
0345418040
-
3D FE Analysis of a Bonded Repair to an F-111 Wing
-
Institute of Engineers, Melbourne, Australia in press
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Callinan, R. J., Sanderson, S. and Keeley, D., '3D FE Analysis of a Bonded Repair to an F-111 Wing', in Proceedings ACAM96, Institute of Engineers, Melbourne, Australia (in press 1996).
-
(1996)
Proceedings ACAM96
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Callinan, R.J.1
Sanderson, S.2
Keeley, D.3
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12
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0344986851
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Bonded Composite Repair of Thin Metallic Materials: Variable Load Amplitude/Temperature Cycling Effects
-
Seville, October 3-5
-
Raizenne, M. D., Benak, T. J., Heath, J. B. R., Simpson, D. L. and Baker, A. A., Bonded Composite Repair of Thin Metallic Materials: Variable Load Amplitude/Temperature Cycling Effects, AGARD Specialists Meeting on Composite Repair of Military Aircraft Structures, Seville, October 3-5, 1994.
-
(1994)
AGARD Specialists Meeting on Composite Repair of Military Aircraft Structures
-
-
Raizenne, M.D.1
Benak, T.J.2
Heath, J.B.R.3
Simpson, D.L.4
Baker, A.A.5
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14
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0010185135
-
Evaluation of Bonded Boron/Epoxy Doublers for Commercial Aircraft Aluminium Structures
-
C. E. Harris (ed.), NASA CP 3274, September
-
Belason, E. B., Rutherford, P. and Miller, M., 'Evaluation of Bonded Boron/Epoxy Doublers for Commercial Aircraft Aluminium Structures', in C. E. Harris (ed.), FAA/NASA Symposium on Advanced Structural Integrity Methods for Airframe Durability and Damage Tolerance, NASA CP 3274, September 1994.
-
(1994)
FAA/NASA Symposium on Advanced Structural Integrity Methods for Airframe Durability and Damage Tolerance
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-
Belason, E.B.1
Rutherford, P.2
Miller, M.3
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16
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0344986843
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to be presented at ISASTI96 Jakarta, June
-
Callinan, R. J., Sanderson, S. and Keeley, D., 'Structural and Theoretical FE Analysis of Bonded Repair to an F-111 Wing', to be presented at ISASTI96 Jakarta, June 1996.
-
(1996)
Structural and Theoretical FE Analysis of Bonded Repair to an F-111 Wing
-
-
Callinan, R.J.1
Sanderson, S.2
Keeley, D.3
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17
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0344124304
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to be presented at ISASTI 96 Jakarta, June
-
Mirabella, L., Galea, S. C. and Sanderson, S., 'Validation of a Bonded Repair to an F-111C Wing: Coupon Testing Program', to be presented at ISASTI 96 Jakarta, June 1996.
-
(1996)
Validation of a Bonded Repair to an F-111C Wing: Coupon Testing Program
-
-
Mirabella, L.1
Galea, S.C.2
Sanderson, S.3
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