Introduction and Overview

Advances in the Bonded Composite Repair of Metallic Aircraft Structure

Volumn 1-2, Issue , 2002, Pages 1-18

  Baker, A A ^a  

^a DEFENCE SCIENCE AND TECHNOLOGY ORGANISATION   (Australia)

Author keywords

[No Author keywords available]

Indexed keywords

ADHESIVES; AIRCRAFT MANUFACTURE; AIRFRAMES; FIBER REINFORCED PLASTICS; FRACTURE MECHANICS; LAMINATED COMPOSITES; NONDESTRUCTIVE EXAMINATION; REINFORCEMENT; REPAIR; STRESS ANALYSIS; TRAINING AIRCRAFT;

APPLICATION TECHNOLOGIES; BONDED COMPOSITE REPAIRS; HEALTH AND SAFETY ISSUES; LINEAR ELASTIC FRACTURE MECHANICS; NON DESTRUCTIVE INSPECTION; RESEARCH AND DEVELOPMENT; STRUCTURAL ADHESIVE BONDINGS; UNITED STATES AIR FORCE;

FIBER BONDING;

EID: 84940844749     PISSN: None     EISSN: None     Source Type: Book    
DOI: 10.1016/B978-008042699-0/50003-6     Document Type: Editorial

References (15)

1. Baker A.A., Jones R. Bonded Repair of Aircraft Structures 1988, Martinus Nijhoff.
2. Aging of U.S. Airforce Aircraft 1997, Publication NMAB-488-2 National Academy Press.
3. Baker A.A. Bonded Composite Repair of Metallic Aircraft Components. Paper 1 in AGARD-CP-550 Composite Repair of Military Aircraft Structures 1994.
4. Baker A.A. On the certification of bonded composite repairs to primary aircraft structures. Proc. 11th Int. Conf. on Comp. Mat. (ICCM-11), Gold Coast, Australia 1997, volume 1:1-24.
5. Simpson D.L., Brooks C.L. Tailoring the structural integrity process to meet the challenges of aging aircraft. Int. J. of Fatigue 1999, 21:S1-S14.
6. Clark G. Corrosion and the management of structural integrity. Structural Integrity for the Next Millennium 1999, EMAS, Washington D.C. J.L. Rudd (Ed.).
7. Nicholas T. Critical issues in high cycle fatigue. Int. J. of Fatigue 1997, 21:S221-S231.
8. Baker A.A. Joining and repair of aircraft composite structures. Composite Engineering Handbook 1997, Chapter 14 in, Marcel Dekker, Inc., Warley. P.K. Mallick (Ed.).
9. Hart-Smith L.J. The Design of Efficient Bolted and Riveted Fibrous Composite Structures 1989, Douglas Paper 8335, July.
10. Swift T. Repairs to damage tolerant aircraft. Proc. Int. Symp. on Structural Integrity of Aging Airplanes 1990, FAA-AIR-01.
11. Fredell R.S., van Barnveld W., Vlot A. Analysis of composite crack patching of fuselage structures: High patch modulus isn't the whole story. SAMPE Int. Symp. 39 1994.
12. Baker A.A., Roberts J.D., Rose L.R.F. Use of joint parameters in estimating the K reduction due to crack patching. Proc. of an Int. Workshop on Defence Applications for Advanced Repair Technology for Metal and Composite Structure 1981, Naval Research Labs.
13. Baker A.A., Rose L.R.F., Walker K.F., et al. Repair substantiation for a bonded composite repair to an F-111 lower wing skin. Applied Composites 1999, 6:251-256.
14. Baker A.A. Issues in the certification of bonded composite patch repairs for cracked metallic aircraft structures. Proc. Int. Conf. on Aircraft Fatigue 1999.
15. Certification of Bonded Structures Action Group 13 Report of the Technical Co-Operation Program 2001.