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Adhesion Associates Pty Ltd
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Publications

  1. Davis, M.J., Shear Stresses in Adhesive Layers of Bonded Step-Lap Sandwich Specimens, ARL Mat Note 109, May 1975.
  2. Davis, M.J., Baker, A.A., Adhesive Strength Tests Using a Step-Lap Sandwich Specimen, ARL Mat. Note 113, Feb. 1976.
  3. Davis, M.J., Stress Intensity Reduction by Strategic Reinforcement, Aust. Fract. Group Conf., Melbourne, Oct. 1978.
  4. Baker, A.A., Davis, M.J., Hawkes, G.A., Repair of Fatigue Cracked Aircraft Structure with Advanced Fibre Composites: Residual Stress and Thermal Fatigue Studies, Proc. 10th. Int. Conf. on Aircraft Fatigue, Brussels, May 1979.
  5. Davis, M.J., Callinan, R.C., Methods for Analysis of Bonded Repairs, Aust. Fract. Group Conf., Melbourne, Oct. 1979.
  6. Baker, A.A., Callinan, R.C., Davis, M.J., Jones, R., Williams, J.G., Application of BFRP Crack Patching to Mirage III Aircraft, Int. Conf. on Composite Matls., Paris, 1980.
  7. Davis, M.J., Repair of Aircraft Structure using High Performance Composite Materials, Thesis for Master of Engineering, (Mech.), Victoria Institute of Colleges, Oct. 1980.
  8. Davis, M.J., Boron Repair to Lower Wing Skin of Mirage, F+W Emmen, Switzerland, ARL Tripartite Mirage Report, March 1981, (Ed. J.J. Sparrow).
  9. Jones, R., Davis, M.J., Callinan, R.C., Mallinson, G.D., Crack Patching:- Analysis and Design, Int. Workshop on Defence Applications of Advanced Repair Technology for Metal and Composite Structures, US Naval Research Labs., Washington, D.C., July, 1981.
  10. Davis, M.J., Roberts, J.D. Procedure for Application of Boron Fibre Reinforced Plastic Patch to the Lower Wing Skin Fuel Decant Point, ARL Tech. Memo. 373, Aug. 1981.
  11. Jones, R., Davis, M.J., Callinan, R.C., Mallinson, G.D., Crack Patching:- Analysis and Design, J. Struct. Mech., Vol 10, No. 2, 1982.
  12. Davis, M.J., Jones, R., Damage Tolerance of Fibre Composite Laminates, Proc. Int. Conf. on Fract. Mech. and Technology, Melbourne, Aug. 1982, (Ed.'s Sih, G.C., Ryan, N.E., Jones, R.), Matinus Nijhoff Publ.
  13. Davis, M.J., Jones R., Damage Tolerance of High Performance Composites, ARL Lecture Series on Composite Materials, ARL Mat. Rept. 114, Oct 1982, Hoskin, B.C., Baker, A.A, (Ed's).
  14. Davis, M.J., Rachinger, A.W., Composite Systems, ARL Lecture Series on Composite Materials, ARL Mat. Rept. 114, Oct 1982, Hoskin, B.C., Baker, A.A, (Ed's).
  15. Davis, M.J., Advanced Fibre Composites, RACI-RMIT Polymer Processing Technology Workshop, RMIT, Melbourne, 1982.
  16. Baker, A.A., Callinan, R.C., Davis, M.J., Jones, R., Williams, J.G., Repair of Mirage III Aircraft using the BFRP Crack Patching Technique, Int. J. of Case Studies in Eng. Mech. and Matls., 1983.
  17. Davis, M.J., Jones R., Damage Tolerance of High Performance Composites, Applications of Composite Materials, AIAA Education Series, 1983 Hoskin, B.C., Baker, A.A, (Ed's).
  18. Davis, M.J., Rachinger, A.W., Composite Systems, Applications of Composite Materials, AIAA Education Series, 1983 Hoskin, B.C., Baker, A.A, (Ed's).
  19. Davis, M.J., Public Service Technical Officer Eligibility Test for the position of Technical Officer, Science - Composite Materials Technology, Defence Training Centre, June 1983. (Unpublished for obvious reasons.)
  20. Davis, M.J., High Performance Fibre Systems for Automotive Applications, SAE Symp. on Plastics in the Automotive Industry, Melbourne, Nov. 1986.
  21. Molent, L., Ferrarotto, P., Davis, M.J., Thermal Strain Survey of an F-111 Wing Pivot Fitting, ARL Struct Tech. Memo. 456, March 1987.
  22. Jones, R., Molent, L., Baker, A.A., Davis, M.J., Bonded Repair of Metallic Components: Thick Sections, Int. Conf. on Anal. and Testing Methodology for Design with Advanced Materials, Montreal, Canada, Aug. 1987, Hoa, S.V., et al (Ed's), Elsiver.
  23. Baker, A.A, Davis, M.J., Recent Advances in Bonded Repair Technology, ANZAAS Bi-Centenary Congress, May 1988.
  24. Baker, A.A, Davis, M.J., Recent Advances in Bonded Repair Technology, AINDT Conference, October 1988.
  25. Modification Order DI (AF) AAP 7214.006-414, which controls the procedures for fabrication, processing and application of the Boron Doubler Modification to F-111 C aircraft, 1989.
  26. Davis, M.J., Repair of Aircraft Structures; Understanding Why Bonded Repairs are Better, 1989 SAMPE Symposium of the Australian Chapter of the Society for Advancement of Materials and Process Engineering, North Ryde, November 1989.
  27. Davis, M.J., Bonded Repairs; Principles and Practice, I.E. Aust. International Conference on Aircraft Damage Assessment and Repair, Melbourne, October 1991.
  28. Davis, M.J., Australian Bonded Repair Management, presented at the 2nd International Workshop on Repair of Aircraft Structures Using Composites, Ottawa, 14-15 September 1993.
  29. Baker, A.A., Chester, R.J., Davis, M.J., Roberts, J.D., Retchford, J.A., Reinforcement of the F-111 Wing Pivot Fitting with a Boron/Epoxy Doubler System, Composites – Material Engineering, 24, (1993) pp 511-521.
  30. Davis, M.J., The Development of an Engineering Standard for Composite Repairs, AGARD SMP Specialists Meeting, Seville, 3-5 October 1994.
  31. Davis, M.J., Kearns, K.J., Wilkin, M.O., Bonded Repair to Cracking in Primary Structure: A Case Study, PICAST2-AAC6 International Aerospace Congress, Melbourne, 20-23 March 1995.
  32. Davis, M.J., A Call for Minimum Standards in Adhesive Bonded Repairs, 3rd. Int. Workshop on Repair of Metallic Structures using Composites, Vancouver, Aug. 1995.
  33. RAAF Standard Engineering C5033, Composite Materials and Adhesive Bonded Repairs, 04 Sep 1995.
  34. Davis, M.J., The Role of Materials and Processes in Defective Aircraft Bonded Structural Repairs, 41st. Int SAMPE Symp. and Exhib., Anaheim, 25-28 Mar 1996.
  35. Hart-Smith, L.J., Redmond, G, Davis, M.J., The Curse of the Nylon Peel Ply, 41st. Int SAMPE Symp. and Exhib., Anaheim, 25-28 Mar 1996.
  36. Hart-Smith, L.J., Davis, M.J., An Object Lesson in False Economies - The Consequences of NOT Updating Repair Procedures for Older Adhesively Bonded Panels, 41st. Int SAMPE Symp. and Exhib., Anaheim, 25-28 Mar 1996.
  37. Davis, M.J., Deficiencies in Regulations for Certification and Continuing Airworthiness of Bonded Structure, Int. Aerospace Congress, Sydney, 25-28 Feb. 1997.
  38. Arnott, D.R., Wilson, A.R, Rider, A.N., Olsson-Jacques, C.L., Lambrianidis, L.T., Pearce, P.J., Davis, M.J., Swan, G., Research Underpinning the Adherend Surface Preparation Aspects of the RAAF Engineering Standard C5033, Int. Aerospace Congress, Sydney, 25-28 Feb. 1997.
  39. Arnott, D.R., Wilson, A.R., Pearce, P.J., Mathys, G., Kindermann, M.R., Camilleri, A., Davis, M.J., Swan, G., Void Development in Aerospace Film Adhesives During Vacuum Bag Cure, Int. Aerospace Congress, Sydney, 25-28 Feb. 1997.
  40. Davis, M.J., The State of Play: Existing Regulations, What Goes Wrong, Why and How Much It Costs, Workshop on Practical Adhesive Bonding for Performance and Durability: Standards and Standardisation, ICCM-11, Brisbane, 11 July 1997.
  41. Davis, M.J., Application Technology and Quality Management, Workshop on Practical Adhesive Bonding for Performance and Durability: Standards and Standardisation, ICCM-11, Brisbane, 11 July 1997.
  42. Davis, M.J., Editor, Proceedings for Workshop on Practical Adhesive Bonding for Performance and Durability: Standards and Standardisation, ICCM-11, Brisbane, 11 July 1997.
  43. Davis, M.J., How Relevant are Load Rate Effects to Realistic Bonded Joints?, The International Conference on Composite Materials - 11, Gold Coast, July 14-18, 1997.
  44. Davis, M.J., Chester, R.J., Perl, D.R., Pomerleau, E., Vallerand, M., Honeycomb Bond and Core Durability Issues; Experiences within CREDP Nations, Aging Aircraft Conference, Williamsberg, VA, Aug 31-Sep 02 1998.
  45. Arnott, D.R., Rider, A.N., Olsson Jacques, C.L., Lambrianidis, L.T., Wilson, A.R., Pearce, P.J., Chester, R.J., Baker, A.A., Morris, C.E.M., Davis, M.J., Swan, G., Bond Durability Performance - The Australian Silane Surface Treatment, 21st Congress of ICAS, Melbourne, 13-18 Sep 98.
  46. Davis, M.J., Bond, D.A., The Importance of Failure Mode Identification in Adhesive Bonded Aircraft Structures and Repairs, The International Conference on Composite Materials – 12, Paris, 05-09 July 1999.
  47. Davis, M.J., Bond, D.A., Towards a Certification Methodology for Adhesively Bonded Structures and Repairs, The Symposium of The International Committee on Aircraft Fatigue – 99, Seattle, 12-16 July 1999.
  48. Davis, M.J., Bond, D.A, Principles and Practices of Adhesive Bonded Structural Joints and Repairs, Int. J. Adhesion, Vol 19 No. 2-3, 1999 pp 91-105.
  49. Davis, M.J., Bond, D.A., Certification of Adhesive Bonds for Construction and Repair, The Aging Aircraft Conference 2000, St. Louis, 15-18 May 2000.
  50. AAP 7021.016-2 Composite and Adhesive Bonded Repairs: Repair Fabrication and Application Aspects, 08 August 2000.
  51. Davis, M.J., Practical Application Technology for Adhesive Bonded Repairs, Advances in the Bonded Composite Repair of Metallic Aircraft Structures, Baker, A.A. Jones, R., Ed's. Matinus Nijhoff publishers, 2000.
  52. Davis, M.J., Janardhana, M. and McKenzie, A, A Rigorous Approach To Certification Of Adhesive Bonded Repairs, MIL HDBK 17 Meeting, Seattle, June 2004.
  53. Davis, M.J., Janardhana M., and Wherrett, A., Adhesive Bonded Repair Technology: Supporting Aging Aircraft, Aging Aircraft Users Forum, Brisbane, May 2006.
  54. Davis, M.J. and Tomblin, J., Best Practice in Adhesive Bonded Structures and Repairs, DOT/FAA/AR – TN06/57, May 2007.
  55. Davis, M.J., and Simpson, R.J (Jim), A Comparison of Adhesive Bonding Processes and Training Standards in Defence and Civil Aviation Industry, Aging Aircraft Users Forum, Brisbane, May 2007.
  56. Davis, M.J. and McGregor, A., Assessing Adhesive Bond Failures: Mixed-Mode Bond Failures Explained, ISASI Australian Safety Seminar, Canberra, June 2010.
  57. Davis, M.J., Safety Risks in Applying Damage Tolerance Analysis to Certification of Adhesively Bonded Structures and Joints, Aircraft Airworthiness and Sustainment Conference, Brisbane, 26-28 July 2011.
  58. Davis, M.J., Is Failure Forensics More Important Than Damage Tolerance in Assessing Defects in Disbonding Structures, 27 May 2013.
  59. Davis, M.J., McGregor, A., The Conditions Where NDI May Not Prevent Failure in Real Bonded Structures, AINDT Inspection and Safety in Aircraft Maintenance Seminar, Brisbane, 05-06 May 2015.
Adhesion Associates Pty. Ltd.
PO Box 4165 SPRINGFIELD CENTRAL   QLD   4300   AUSTRALIA