Validation of Stress Intensity Estimations in Patched Panels

Advances in the Bonded Composite Repair of Metallic Aircraft Structure

Volumn 1-2, Issue , 2002, Pages 517-530

  Aktepe, B ^a   Baker, A A ^a  

^a DEFENCE SCIENCE AND TECHNOLOGY ORGANISATION   (Australia)

Author keywords

[No Author keywords available]

Indexed keywords

CRACK TIPS; FATIGUE CRACK PROPAGATION; GROWTH RATE;

AVERAGE STRAIN; DESIGN MODELS; FATIGUE CRACK GROWTH BEHAVIOR; FATIGUE EXPERIMENTS; FINITE-ELEMENT APPROACH; SEVERAL VARIABLES; STRESS INTENSITY; VERTICAL DIRECTION;

FATIGUE OF MATERIALS;

EID: 84940846279     PISSN: None     EISSN: None     Source Type: Book    
DOI: 10.1016/B978-008042699-0/50020-6     Document Type: Chapter

References (9)

1. Bonded Repair of Aircraft Structures 1988, Martinus Nijhoff Publishers, Albuquerque, NM. A.A. Baker, R. Jones (Eds.).
2. Baker A.A. Fatigue studies related to certification of composite crack patching for primary metallic structure. Proc. of the FAA/NASA Symp. on Continued Airworthiness of Aircraft Structures 1996.
3. Rose L.R.F. Theoretical analysis of crack patching. Bonded Repair of Aircraft Structures 1988, 107-173. Chapter 6, Martinus Nijhoff, Dordrecht. A.A. Baker, R. Jones (Eds.).
4. Kondo Y. Stress intensity factor measurement in service condition using "K-gauge". VI Inte. Congress on Experimental Mechanics 1988. Portland, Oregon, June 6-10
5. Miyake S., Nawa Y., Kondo Y., et al. Application of the "K-gauge" to Aircraft Structural Testing. Proc. of ICAF 1989.
6. Westergaard H.M. Bearing pressures and cracks. J. of Applied Mechanics 1939, A.
7. Wang C.H., Rose L.R.F. Bonded repair of cracks under mixed mode loading. Int. J. of Solids 1998, 35:2748-2773.
8. Ryall T.G., Wong A.K. Design of a focal-plane array thermographic system for stress analysis. Experimental Mechanics 1995, 35:144-147. June.
9. Broek D. Elementary Engineering Fracture Mechanics 1986, Martinus Nijhoff Publishers, Dordrecht.