Aging aircraft/fatique site list
Aging aircraft/fatique site list
2
amorrison (Mechanical)
(OP)
This started out as a simple google search that got out of hand! :(
Hopefully it is useful to someone.
For 1999 http://www.galaxyscientific.com/agingaircraft/agen...#
For 2000 ?
For 2001 www.agingaircraft2001.com/papers/CombinedPapers.pd...
For 2002 http://www.galaxyscientific.com/agingaircraft2002/
For 2003 ?
For 2004 ?
For 2005 http://www.agingaircraft.utcdayton.com/pages/call....
Additional materials:
RTO-MP-079(II) Ageing Mechanisms and Control Specialists' Meeting on Life Management Techniques for Ageing Air Vehicles
Available at http://www.rta.nato.int/Rdp.asp?RDP=RTO-MP-079(II)
RTO-EN-015 Aging Aircraft Fleets: Structural and Other Subsystem Aspects
Available at http://www.rta.nato.int/Rdp.asp?RDP=RTO-EN-015
Assessment of Probabilistic Certification Methodology for Composite Structures : Final Report
Available at http://www.tc.faa.gov/its/worldpac/techrpt/ar00-74...
Characterization of In-Plane, Shear-Loaded Adhesive Lap Joints: Experiments and Analysis : Final Report
Available from: http://www.tc.faa.gov/its/worldpac/techrpt/ar03-21...
Damage Tolerance and Durability of Selectively Stitched, Stiffened Panels : Final Report
Available from: http://www.tc.faa.gov/its/worldpac/techrpt/ar03-46...
Failure Modeling of Titanium 6A1-4V and Aluminum 2024-T3 with the Johnson-Cook Material Model
Available from: http://www.tc.faa.gov/its/worldpac/techrpt/ar03-57...
Fatigue Resource Directory (FReDi)
Available from: http://human-factors.arc.nasa.gov/zteam/fredi/
Federal Aviation Administration : Aging Aircraft Program
Available from: http://aar400.tc.faa.gov/Programs/AgingAircraft/in...
Federal Aviation Administration : Aging Systems Program
Available from: http://aar400.tc.faa.gov/agingsystems/
Federal Aviation Administration Technical Reports
Available from: http://www.faa.gov/aar/techrep.htm
Full-Scale Testing and Analysis of Fuselage Structure Containing : Final Report Multiple Cracks
Available from: http://www.tc.faa.gov/its/worldpac/techrpt/ar01-46...
Guidelines for Analysis, Testing, and Nondestructive Inspection of Impact-Damaged Composite Sandwich Structures : Final Report
Available from: http://www.tc.faa.gov/its/worldpac/techrpt/ar02-12...
Investigation of Adhesive Behavior in Aircraft Applications : Final Report
Available from: http://www.tc.faa.gov/its/worldpac/techrpt/ar01-57...
NTIAC Newsletter (non destructive testing)
Available from: http://www.ntiac.com/newslist.html
Poulter Laboratory : Aircraft Safety Research
Available from: http://www.sri.com/poulter/air_safety/air_safety.h...
Probabilistic Design of Damage Tolerant Composite Aircraft Structures : Final Report
Available from: http://www.tc.faa.gov/its/worldpac/techrpt/ar01-55...
Proceedings of the FAA-NASA Symposium on the Continued Airworthiness of Aircraft Structures : Vol. 1
Available from: http://www.tc.faa.gov/its/worldpac/techrpt/ar97-2-...
FATIGUE ASSESSMENT OF AN AGING AIRCRAFT'S WING UNDER COMPLEX MULTIAXIAL SPECTRUM LOADING
Available at www.vtt.fi/tuo/33/pdf/icbmff7_ 2004_backstrom_etal_hw_wing.pdf
Hopefully it is useful to someone.
For 1999 http://www.galaxyscientific.com/agingaircraft/agen...#
For 2000 ?
For 2001 www.agingaircraft2001.com/papers/CombinedPapers.pd...
For 2002 http://www.galaxyscientific.com/agingaircraft2002/
For 2003 ?
For 2004 ?
For 2005 http://www.agingaircraft.utcdayton.com/pages/call....
Additional materials:
RTO-MP-079(II) Ageing Mechanisms and Control Specialists' Meeting on Life Management Techniques for Ageing Air Vehicles
Available at http://www.rta.nato.int/Rdp.asp?RDP=RTO-MP-079(II)
RTO-EN-015 Aging Aircraft Fleets: Structural and Other Subsystem Aspects
Available at http://www.rta.nato.int/Rdp.asp?RDP=RTO-EN-015
Assessment of Probabilistic Certification Methodology for Composite Structures : Final Report
Available at http://www.tc.faa.gov/its/worldpac/techrpt/ar00-74...
Characterization of In-Plane, Shear-Loaded Adhesive Lap Joints: Experiments and Analysis : Final Report
Available from: http://www.tc.faa.gov/its/worldpac/techrpt/ar03-21...
Damage Tolerance and Durability of Selectively Stitched, Stiffened Panels : Final Report
Available from: http://www.tc.faa.gov/its/worldpac/techrpt/ar03-46...
Failure Modeling of Titanium 6A1-4V and Aluminum 2024-T3 with the Johnson-Cook Material Model
Available from: http://www.tc.faa.gov/its/worldpac/techrpt/ar03-57...
Fatigue Resource Directory (FReDi)
Available from: http://human-factors.arc.nasa.gov/zteam/fredi/
Federal Aviation Administration : Aging Aircraft Program
Available from: http://aar400.tc.faa.gov/Programs/AgingAircraft/in...
Federal Aviation Administration : Aging Systems Program
Available from: http://aar400.tc.faa.gov/agingsystems/
Federal Aviation Administration Technical Reports
Available from: http://www.faa.gov/aar/techrep.htm
Full-Scale Testing and Analysis of Fuselage Structure Containing : Final Report Multiple Cracks
Available from: http://www.tc.faa.gov/its/worldpac/techrpt/ar01-46...
Guidelines for Analysis, Testing, and Nondestructive Inspection of Impact-Damaged Composite Sandwich Structures : Final Report
Available from: http://www.tc.faa.gov/its/worldpac/techrpt/ar02-12...
Investigation of Adhesive Behavior in Aircraft Applications : Final Report
Available from: http://www.tc.faa.gov/its/worldpac/techrpt/ar01-57...
NTIAC Newsletter (non destructive testing)
Available from: http://www.ntiac.com/newslist.html
Poulter Laboratory : Aircraft Safety Research
Available from: http://www.sri.com/poulter/air_safety/air_safety.h...
Probabilistic Design of Damage Tolerant Composite Aircraft Structures : Final Report
Available from: http://www.tc.faa.gov/its/worldpac/techrpt/ar01-55...
Proceedings of the FAA-NASA Symposium on the Continued Airworthiness of Aircraft Structures : Vol. 1
Available from: http://www.tc.faa.gov/its/worldpac/techrpt/ar97-2-...
FATIGUE ASSESSMENT OF AN AGING AIRCRAFT'S WING UNDER COMPLEX MULTIAXIAL SPECTRUM LOADING
Available at www.vtt.fi/tuo/33/pdf/icbmff7_ 2004_backstrom_etal_hw_wing.pdf





RE: Aging aircraft/fatique site list
This would make an excellent FAQ (to prevent it from getting lost in the flow of subsequent messages).
Steven Fahey, CET
"Simplicate, and add more lightness" - Bill Stout