Case History: F-111 Lower Wing Skin Repair Substantiation

Advances in the Bonded Composite Repair of Metallic Aircraft Structure

Volumn 2-2, Issue , 2002, Pages 797-812

  Walker, K F ^a   Rose, L R F ^a  

^a DEFENCE SCIENCE AND TECHNOLOGY ORGANISATION   (Australia)

Author keywords

[No Author keywords available]

Indexed keywords

FATIGUE TESTING; FIBER OPTIC SENSORS; REPAIR; SAFETY ENGINEERING; SUPERSONIC AIRCRAFT;

3D-FINITE ELEMENT ANALYSIS; BONDED COMPOSITE REPAIRS; ENGINEERING STANDARDS; F-111 AIRCRAFTS; INDEPENDENT ANALYSIS; OPERATIONAL USAGE; ROYAL AUSTRALIAN AIR FORCES; VALIDATION PROCESS;

WINGS;

EID: 84940866840     PISSN: None     EISSN: None     Source Type: Book    
DOI: 10.1016/B978-008042699-0/50029-2     Document Type: Chapter

References (15)

1. Composite Materials and Adhesive Bonded Repairs, RAAF Standard Engineering C5033 Issue 1 1995.
2. Bonded Repair of Aircraft Structures, Martinus Nijhoff 1988, A.A. Baker, R. Jones (Eds.).
3. Baker A.A. Bonded Composite Repair of Metallic Aircraft Components - Overview of Australian Activities, AGARD Specialist Meeting on Composite Repair of Military Aircraft Structures 1994.
4. McHenry H.I., Key R.E. The F-111 Logic: Familiar Materials; Proven Processes. Metal Progress 1968, 93(3):62-68.
5. Callinan R.J., Sanderson S., Keeley D. Finite Element Analysis of an F-111 Lower Wing Skin Fatigue Crack Repair 1997, DSTO-TN-0067, January.
6. Keeley D., Callinan R., Sanderson S. A Validated Finite Element Model of an F-111 Lower Wing Skin Structural Detail at Forward Auxiliary Spar Station 281.28 1996, DSTO-TN-0046, June.
7. Keeley D., Callinan R., Sanderson S. Sensitivity Study of an AMRL Finite Element Model of the F-111 Lower Wing Skin Structural Detail at Forward Auxiliary Spar Station (FASS) 1996, 281.28, DSTO-TN-0060, September.
8. Callinan R.J., Sanderson S., Keeley D. Finite Element Analysis of an F-111 Lower Wing Skin Fatigue Crack Repair 1997, DSTO-TN-0067, January.
9. Walker K., Swanton G. Static and Fatigue Loading Development for an F-111 Bonded Composite Repair Substantiation 1996, DSTO-TN-0063, November.
10. Lincoln J.W. Challenges for the aircraft structural integrity program. Proc. FAA/NASA Symp. on Advanced Structural Integrity Methods for Airframe Durability and Damage Tolerance 1994, NASA CP 3274, September. C.E. Harris (Ed.).
11. Raizenne M.D., Benak T.J., Heath J.B.R. Bonded Composite Repair of Thin Metallic Materials: Variable Load Amplitude/Temperature Cycling Effects 1994, Report LTR-ST-1979, August, Institute for Aerospace Research, United Kingdom.
12. Belason E.B. Status of Bonded Boron/Epoxy Doublers for Military and Commercial Aircraft Structures, AGARD Specialists Meeting on Composite Repair of Military Aircraft Structures 1994.
13. Belason E.B., Rutherford P., Miller M. Evaluation of Bonded Boron/Epoxy Doublers for Commercial Aircraft Aluminium Structures. FAA/NASA Symposium on Advanced Structural Integrity Methods for Airframe Durability and Damage Tolerance 1994, NASA CP 3274, September. C.E. Harris (Ed.).
14. Boykett R., Walker K. F-111C Lower Wing Skin Bonded Composite Repair Substantiation Testing 1996, DSTO-TR-0480, November.
15. Walker K., Boykett R. Repair Substantiation Fatigue Testing Including Temperature and Frequency Effects for a Bonded Composite Repair to an F-111 Lower Wing Skin. Presented at the USAF ASIP Conference 1996.