Widespread Fatigue Damage Assessment of Jet Transport Structures
Validation of Life Prediction Models from Representative Testings on Aluminium Alloy Specimens
Using the Initial Flaw Concept in Current and Future Aircraft Certifications
US Air Force Risk Analysis Approach for Aging Aircraft
Toward the Supportable and Durable Aircraft Fuselage Structure
Towards a Certification Methodology for Adhesively Bonded Structures and Repairs
Toward a Damage Tolerance Evaluation of Helicopter Composite Components
The Use of Field Inspection Data in the Performance Measurement of Nondestructive Inspections
The Royal New Zealand Air Force Andover C.MK.1 Loads Environment Spectrum Survey (L/ESS)
The Role of Fretting Fatigue in Aircraft Rivet Hole Cracking
The Role of Corrosion Pillowing in NDI and in the Structural Integrity of Fuselage Joints
The Role of Airline's Maintenance on Continuing Airworthiness of Aging Aircraft
Thermographic NDE Application for Quantitative Disbond and Corrosion Detection in Aircraft Skin
The Mechanism of Fatigue - a Critical Factor in the Prediction of the Life of Structures
The Influence of Residual Stress on the Design and Damage Tolerance of Welded Aircraft Structures