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2
- #1
amorrison
Mechanical
- Dec 21, 2000
- 605
This started out as a simple google search that got out of hand!
Hopefully it is useful to someone.
For 1999
For 2000 ?
For 2001
For 2002
For 2003 ?
For 2004 ?
For 2005
Additional materials:
RTO-MP-079(II) Ageing Mechanisms and Control Specialists' Meeting on Life Management Techniques for Ageing Air Vehicles
Available at
RTO-EN-015 Aging Aircraft Fleets: Structural and Other Subsystem Aspects
Available at
Assessment of Probabilistic Certification Methodology for Composite Structures : Final Report
Available at
Characterization of In-Plane, Shear-Loaded Adhesive Lap Joints: Experiments and Analysis : Final Report
Available from:
Damage Tolerance and Durability of Selectively Stitched, Stiffened Panels : Final Report
Available from:
Failure Modeling of Titanium 6A1-4V and Aluminum 2024-T3 with the Johnson-Cook Material Model
Available from:
Fatigue Resource Directory (FReDi)
Available from:
Federal Aviation Administration : Aging Aircraft Program
Available from:
Federal Aviation Administration : Aging Systems Program
Available from:
Federal Aviation Administration Technical Reports
Available from:
Full-Scale Testing and Analysis of Fuselage Structure Containing : Final Report Multiple Cracks
Available from:
Guidelines for Analysis, Testing, and Nondestructive Inspection of Impact-Damaged Composite Sandwich Structures : Final Report
Available from:
Investigation of Adhesive Behavior in Aircraft Applications : Final Report
Available from:
NTIAC Newsletter (non destructive testing)
Available from:
Poulter Laboratory : Aircraft Safety Research
Available from:
Probabilistic Design of Damage Tolerant Composite Aircraft Structures : Final Report
Available from:
Proceedings of the FAA-NASA Symposium on the Continued Airworthiness of Aircraft Structures : Vol. 1
Available from:
FATIGUE ASSESSMENT OF AN AGING AIRCRAFT'S WING UNDER COMPLEX MULTIAXIAL SPECTRUM LOADING
Available at 2004_backstrom_etal_hw_wing.pdf
Hopefully it is useful to someone.
For 1999
For 2000 ?
For 2001
For 2002
For 2003 ?
For 2004 ?
For 2005
Additional materials:
RTO-MP-079(II) Ageing Mechanisms and Control Specialists' Meeting on Life Management Techniques for Ageing Air Vehicles
Available at
RTO-EN-015 Aging Aircraft Fleets: Structural and Other Subsystem Aspects
Available at
Assessment of Probabilistic Certification Methodology for Composite Structures : Final Report
Available at
Characterization of In-Plane, Shear-Loaded Adhesive Lap Joints: Experiments and Analysis : Final Report
Available from:
Damage Tolerance and Durability of Selectively Stitched, Stiffened Panels : Final Report
Available from:
Failure Modeling of Titanium 6A1-4V and Aluminum 2024-T3 with the Johnson-Cook Material Model
Available from:
Fatigue Resource Directory (FReDi)
Available from:
Federal Aviation Administration : Aging Aircraft Program
Available from:
Federal Aviation Administration : Aging Systems Program
Available from:
Federal Aviation Administration Technical Reports
Available from:
Full-Scale Testing and Analysis of Fuselage Structure Containing : Final Report Multiple Cracks
Available from:
Guidelines for Analysis, Testing, and Nondestructive Inspection of Impact-Damaged Composite Sandwich Structures : Final Report
Available from:
Investigation of Adhesive Behavior in Aircraft Applications : Final Report
Available from:
NTIAC Newsletter (non destructive testing)
Available from:
Poulter Laboratory : Aircraft Safety Research
Available from:
Probabilistic Design of Damage Tolerant Composite Aircraft Structures : Final Report
Available from:
Proceedings of the FAA-NASA Symposium on the Continued Airworthiness of Aircraft Structures : Vol. 1
Available from:
FATIGUE ASSESSMENT OF AN AGING AIRCRAFT'S WING UNDER COMPLEX MULTIAXIAL SPECTRUM LOADING
Available at 2004_backstrom_etal_hw_wing.pdf