Bonded composite repair of fatigue-cracked primary aircraft structure
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Abstract
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Research context
OpenAlex topics: Mechanical Behavior of Composites · Fatigue and fracture mechanics · Structural Behavior of Reinforced Concrete
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References (29)
Show source-provided references
1. Baker AA. Joining and repair of aircraft composite structures. In: Mallick PK, editor. Part 14 Composite engineering handbook. New York: Marcel Dekker, 1997
2. Baker AA. Crack patching. In: Baker AA, Jones R, editors. Bonded repair of aircraft structures. Dordrecht: Martinus Nijhoff, 1988: pp. 107–73 [chapter 6: Experimental studies, practical applications]10.1007/978-94-009-2752-0_6 ↗
3. Repair of cracked or defective metallic aircraft components with advanced fibre composites – an overview of Australian work10.1016/0263-8223(84)90025-4 ↗
4. Baker AA. Bonded composite repair of metallic aircraft components. AGARD-CP-550 Composite Repair of Military Aircraft Structures, Paper 1, 199410.1002/9781118097298.weoc017 ↗
5. Kerr A. Certification of bonded repairs. In: Proceedings of the USAF Aircraft Structural Integrity Program (ASIP), San Antonio, 1998
6. Baker AA. On the certification of bonded composite repairs to primary aircraft structures. In: Proceedings of the Eleventh International Conference on Composite Materials (ICCM-11), Gold Coast, Australia, 1997
7. Baker AA, Rose LRF, Walker KF, Wilson ES. Repair substantiation for a bonded composite repair to an F-111 lower wing skin. Appl Compos 1999;6:251–6710.1023/A:1008805813470 ↗
8. Davis M. The development of an engineering standard for composite repairs, AGARD-CP-550 Composite Repair of Military Aircraft Structures, Paper 24, 1994
9. Royal Australian Air Force Engineering Standard for Composite Materials and Adhesive Bonded Repairs, No. C5033 Issue 1. Department of Defence, Australia
10. Baker AA. Fatigue studies related to certification of composite crack patching for primary metallic structure. In: Proceedings of the FAA/NASA Symposium on Continued Airworthiness of Aircraft Structures, Atlanta USA, pp. 313–30
11. Hart-Smith LJ. An engineer’s viewpoint on design and analysis of aircraft structural joints, Douglas Paper MDC 91K0067. In: Proceedings of the International Conference on Aircraft Damage Assessment and Repair, Australian Institute of Engineers, Melbourne, Australia, August 1991
12. Tran-Cong T, Heller M. Reduction in adhesive shear strains at the ends of bonded reinforcements, DSTO, AMRL Research Report, DSTO-RR-0115, 1997
13. Naboulsi S, Mall S, Denny JJ. Analysis of fatigue crack growth in imperfectly bonded composite patch repair of cracked aluminium panels. In: Proceedings of the International Conference on Aeronautical Fatigue 1997 (ICAF97)10.2514/6.1997-1363 ↗
14. Development of a generic repair joint for certification of bonded composite repairs10.1016/S0143-7496(98)90028-8 ↗
15. Rose LRF. In: Baker AA, Jones R, editors. Bonded repair of aircraft structures. Dordrecht: Martinus Nijhoff, 1988: pp. 107–73 [chapter 6: Theoretical analysis of crack patching]
16. Modelling fatigue crack growth of patched cracks
17. Newman JC, FASTRANII – A fatigue crack growth structural analysis program, NASA Technical Memorandum 104195, NASA Langley Research Centre, 1992
18. Raizenne MD, Heath JBR, Benak T. TTCP PTP-4 Collaborative test program – variable amplitude loading of thin metallic materials repaired with composite patches, Laboratory Technical Report, LTR-ST-1662, National Aeronautical Establishment, Ottawa, Canada, 1988
19. Baker AA, Aktepe B. Sensor techniques to validate stress intensity models in cracked metallic panels repaired with bonded composite patches. In: Proceedings of the International Conference on Composite Materials (ICCM 12) Paris, 1999
20. Minimum surface treatments for adhesively bonded repairs10.1016/0143-7496(92)90026-R ↗
21. Kinloch AJ. Adhesion and adhesives: science and technology. London: Chapman & Hall, 1987 [chapter 7 – Fracture mechanics of adhesive joints]10.1007/978-94-015-7764-9 ↗
22. Kindermann MR, Wilson AR, Arnott DR. A multiple constant displacement-rate tensile testing machine. Measurement Sci Technol 1997;8:390–9710.1088/0957-0233/8/4/005 ↗
23. Olsson-Jacques CL, Arnott DR, Lambrianidis LT, Wilson AR, Kindermann MR, Theodossiou G. Toward quality monitoring of adherend surfaces prior to adhesive bonding in aircraft repairs. In: Proceedings of the International Aerospace Congress 1997 Seventh Australian Aeronautical Conference, Institution of Engineers Australia, 24–27 February, 1997, Sydney, Australia, pp. 511–20
24. Baker AA, Galea SC, Powlesland IG. A smart patch approach for bonded composite repairs to primary airframe structures. In: Proceedings of the Second Joint FAA/DOD/NASA Conference on Aging Aircraft, Williamsberg VA, 1998
25. The development of a boron/epoxy doubler system for the f111 wing pivot fitting – materials engineering aspects10.1016/0010-4361(93)90021-Y ↗
26. Web site: http://www.acq.osd.mil/es/dut/, Micromechanical Systems Opportunities
27. Chester R. Life extension of F/A-18 inboard aileron hinges by shape optimisation and composite reinforcement, DSTO – TR- 0699, January 1999
28. Baker A, Meadows L. Air force research area critical issues paper: smart materials and structures for military airframes. Defence Science and Technology Report DSTO-GD-0176, May 1998
29. Schweinberg W, Jenson R, Fiebeg J. Advanced composite repairs of the C141 wing structure, International Conference of Composite Materials ICCM 10, 1995