Repair Substantiation for a Bonded Composite Repair to F111 Lower Wing Skin
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Abstract
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Research context
OpenAlex topics: Probabilistic and Robust Engineering Design · Fatigue and fracture mechanics · Mechanical Failure Analysis and Simulation
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References (17)
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1. Baker, A. A. and Jones, R. (eds), Bonded Repair of Aircraft Structures, Martinus Nijhoff, 1988.10.1007/978-94-009-2752-0 ↗
2. Baker, A. A., Bonded Composite Repair of Metallic Aircraft Components — Overview of Australian Activities, AGARD Specialists Meeting on Composite Repair of Military Aircraft Structures, Seville, October 3–5, 1994.
3. Davis, M. J., The Development of an Engineering Standard for Composite Repairs, AGARD Specialists Meeting on Composite Repair of Military Aircraft Structures, Seville, October 3–5, 1994.
4. Composite Materials and Adhesive Bonded Repairs, RAAF Standard Engineering C5033, Draft, January 1994.
5. 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.
6. McHenry, H. I. and Key, R. E., 'The F-111 Logic: Familiar Materials; Proven Processes', Metal Progress 93(3), 1968, 62-68.
7. 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.
8. Callinan, R. J. and Sanderson, S., Analysis of RAAF Bonded Repair to F-111 Lower Skin, Part 1 — Uncracked Analysis, (M1/9/136).
9. 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).
10. Broek, D., The Practical Use of Fracture Mechanics, Kluwer Academic Publishers, Dordrecht, 1989.10.1007/978-94-009-2558-8 ↗
11. Lincoln, J. W., 'Challenges for the Aircraft Structural Integrity Program', in C. E. Harris (ed.), Proceedings FAA/NASA Symposium on Advanced Structural Integrity Methods for Airframe Durability and Damage Tolerance, NASA CP 3274, September 1994.
12. 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.
13. Belason, E. B., Status of Bonded Boron/Epoxy Doublers for Military and Commercial Aircraft Structures, AGARD Specialists Meeting on Composite Repair of Military Aircraft Structures, Seville, October 3–5, 1994.10.4271/951145 ↗
14. 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 1994.10.4271/951145 ↗
15. Rose, L. R. F., Theoretical Analysis of Crack Patching, Chapter 5 in [1].
16. 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 ISASTI 96 Jakarta, June 1996.
17. 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.