Dr. Cong Duong received a B.S. degree in Aerospace Engineering from California Polytechnic State University, Pomona (1984), a S.M. degree in Aeronautics and Astronautics from Massachusetts Institute of Technology (1986), and a Ph.D. in Applied Mechanics from California Institute of Technology (1994). He is currently an Associated Technical Fellow of the Boeing Company where he has been working in the durability and damage tolerance group for sixteen years. From 1999-2005, he was a principal investigator of the USAF funded Composite Repair of Aircraft Structures (CRAS) program. Under that program, he had developed and implemented analytical and computational methods for design and analysis of bonded repairs over metallic aircraft structures. He is currently developing analytical methods for determining the allowable damage limits and the allowable repair limits on airframe of the new Boeing 787. He has published about twenty papers in peer-review journals, mostly on the subjects of bonded repairs, bonded joints and fracture mechanics.
1. Introduction
2. Theory of Bonded Doublers and Bonded Joints
3. Fundamental Concept of Crack Patching
4. Mathematical Theory of Supported One-Sided Crack Patching or Two-Sided
Crack Patching
5. Approximate Theory of Unsupported One-Sided Crack Patching
6. Analytical Approach to Repairs of Corrosion Grind-Outs
7. Bond Line Analysis at Patch Ends
8. Fatigue Crack Growth Analyses of Repaired Structures
9. A Preliminary Design Approach for Crack Patching
10. A Preliminary Design Approach for Corrosion Repairs
11. Experimental Verification of Analytical Methods
12. Repair of Sonic Fatigue
13. Repair Analysis Methods Accounting for Secondary Effects
14. Concluding Remarks
