Aerospace

Adhesive Bonding: Science, Technology and Applications

Volumn , Issue , 2005, Pages 489-527

  Hart Smith, L J ^a  

^a BOEING COMPANY   (United States)

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[No Author keywords available]

Indexed keywords

EID: 34250884886     PISSN: None     EISSN: None     Source Type: Book    
DOI: 10.1533/9781845690755.3.489     Document Type: Chapter

References (25)

1. Hart-Smith L.J. Analysis and Design of Advanced Composite Bonded Joints 1974, NASA Langley Contract Report NASA CR-2218, January 1973; reprinted, complete, August.
2. Gosse J.H., Christensen S. Strain Invariant Failure Criteria for Polymers in Composite Materials 2001, AIAA paper AIAA-2001-1184, presented to 42nd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference Seattle, Washington 16-19 April.
3. Krieger R.B. Stress Analysis Concepts for Adhesive Bonding of Aircraft Primary Structure. Adhesively Bonded Joints: Testing, Analysis and Design, ASTM STP 981 1988, 264-275. American Society for Testing and Materials, Philadelphia. W.S. Johnson (Ed.).
4. Hart-Smith L.J. The Bonded Lap-Shear Test Coupon - Useful for Quality Assurance, but Dangerously Misleading for Design Data 1993, 239-246. McDonnell Douglas Paper MDC 92K0922, presented to 38th International SAMPE Symposium & Exhibition, Anaheim, California, May 10-13.
5. de Bruyne N A, 'Fundamentals of Adhesion', in Bonded Aircraft Structures, a collection of papers given in 1957 at a conference in Cambridge, England, Bonded Structures, Ltd., Duxford, England, pp. 1-9.
6. Schliekelmann R.J. Adhesive Bonding and Composites. Progress in Science and Engineering of Composites 1983, Vol 1:63-78. Fourth International Conference on Composite Materials, North-Holland. T. Hayashi, K. Kawata, S. Umekawa (Eds.).
7. 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 1996, 279-290. McDonnell Douglas Paper MDC 95K0074, presented to 41st International SAMPE Symposium and Exhibition, Anaheim, March 25-28.
8. Marceau J.A., Moji Y., McMillan J.C. A Wedge Test for Evaluating Adhesive Bonded Surface Durability. Adhesives Age 1977, 28-34.
9. Adhesive Bonding of Aluminum Alloys 1985, 241-321. Marcel Dekker, New York. E.W. Thrall, R.W. Shannon (Eds.).
10. Hart-Smith L.J., Redmond G., Davis M.J. The Curse of the Nylon Peel Ply 1996, 303-317. McDonnell Douglas Paper MDC 95K0072, presented to 41st International SAMPE Symposium and Exhibition, Anaheim, March 25-28.
11. Mahoney C.L. Fundamental Factors Influencing the Performance of Structural Adhesives. Internal Report 1988, Dexter Adhesives & Structural Materials Division, The Dexter Corporation.
12. Myhre S.H., Labor J.D., Aker S.C. Moisture Problems in Advanced Composite Structural Repair. Composites 1982, 13:289-297. 3, July.
13. Bardis J. Effects of Surface Preparation on Long-term Durability of Composite Adhesive Bonds 2001, Proc. MIL-HDBK-17 Meeting, Santa Barbara, California, October 16.
14. Hart-Smith L.J. Adhesive-Bonded Double-Lap Joints 1973, NASA Langley Contract Report NASA CR-112235, January 1973; 'Adhesive-Bonded Single-Lap Joints', NASA Langley Contract Report NASA CR-112236, January 1973; 'Adhesive-Bonded Scarf and Stepped-Lap Joints', NASA Langley Contract Report NASA CR-112237, January 1973; and 'Non-Classical Adhesive-Bonded Joints in Practical Aerospace Construction', NASA Langley Contract Report NASA CR-112238, January.
15. Hart-Smith L.J. Design Methodology for Bonded-Bolted Composite Joints. USAF Contract Report AFWAL-TR-81-3154 1982, 2 vols. February, See also 'Bonded-Bolted Composite Joints', Douglas Paper 7398, presented to AIAA/ASME/ASCE/AHS 25th Structures, Structural Dynamics and Materials Conference, Palm Springs, California, May 14-16, 1984; published in Jnl. Aircraft, 22, 1985, 993-1000.
16. Hart-Smith L.J. A Demonstration of The Versatility of Rose's Closed-Form Analyses for Bonded Crack Patching. 2002: A Materials and Processes Odyssey 2001, 1118-1134. Boeing Paper MDC 00K0104, presented to 46th International SAMPE Symposium and Exhibition, Long Beach, California. May 6-10, in Proceedings.
17. Hart-Smith L J, 'The Goland And Reissner Bonded Lap Joint Analysis Revisited Yet Again - But This Time Essentially Validated', Boeing Paper MDC 00K0036, to be published.
18. Hart-Smith L.J. Explanation of Delamination of Bonded Patches Under Compressive Loads, Using New Simple Bonded Joint Analyses 2001, presented to 3rd Quarterly CRAS Review, in conjunction with Fifth Joint DoD/FAA/NASA Conference on Aging Aircraft, Kissimmee, Florida, September 10-13.
19. Hart-Smith L.J. Adhesive Layer Thickness and Porosity Criteria for Bonded Joints 1982, USAF Contract Report AFWAL-TR-82-4172, December.
20. Hart-Smith L.J. Adhesive-Bonded Joints for Composites Phenomenological Considerations 1978, 163-180. Douglas Paper 6707, presented to Technology Conferences Associates Conference on Advanced Composites Technology, El Segundo, California, March 14-16, reprinted as 'Designing Adhesive Bonds', in Adhesives Age 21, October 1978, pp. 32-37.
21. Hart-Smith L.J., Strindberg G. Developments in Adhesively Bonding the Wings of the SAAB 340 and 2000 Aircraft. Proceedings 1995, 2:545-550. McDonnell Douglas Paper MDC 94K0098, presented to 2nd PICAST & 6th Australian Aeronautical Conference, Melbourne, Australia, March 20-23, abridged version, full paper published in Proc. Instn. Mech. Engrs, Part G, Journal of Aerospace Engineering, 211, 1997, pp. 133-156.
22. Hart-Smith L.J. Reliable Nondestructive Inspection of Adhesively Bonded Metallic Structures Without Using Any Instruments 1995, 1124-1133. McDonnell Douglas Paper MDC 94K0091, presented to 40th International SAMPE Symposium and Exhibition, Anaheim, May 8-11.
23. Hart-Smith L.J. Interface Control - The Secret to Making DFMA® Succeed 1997, 1-10. McDonnell Douglas Paper No. MDC 96K0132, presented at SAE Aerospace Manufacturing Technology Conference & Exposition, Seattle, June 2-5, SAE Paper No. 972191.
24. Hart-Smith L.J. Is It Really More Important that Paint Stays Stuck on the Outside of an Aircraft than that Glue Stays Stuck on the Inside? 2003, Boeing Paper PWMD02-0209, presented to 26th Annual Meeting of the Adhesion Society, Myrtle Beach, South Carolina, February 23-26.
25. Bonded Repairs of Aircraft Structures 1987, 77-106. Martinus Nijhoff Publishers. A.A. Baker, R. Jones (Eds.).